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Research Article Fuzzy Control for Seismic Protection of Semiactive Base-Isolated Structures Subjected to Near-Fault Earthquakes Dahai Zhao and Yongxing Li School of Civil Engineering and Mechanics, Yanshan University, No. 438 Hebei Road, Qinhuangdao, Hebei, China Correspondence should be addressed to Dahai Zhao; [email protected] Received 22 October 2015; Accepted 6 December 2015 Academic Editor: Filippo Ubertini Copyright © 2015 D. Zhao and Y. Li. is is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited. is paper proposes a new fuzzy logic controller, which is designed for seismic protection of base-isolated structures utilizing piezoelectric friction damper against near-fault earthquakes for different ground sites. According to the elastic design spectrum that Eurocode 8 recommends, one 5% damped elastic design spectrum for Chi-Chi earthquake is proposed to generate artificial earthquakes of different ground sites. e proposed controller employs a hierarchic fuzzy control algorithm, in which a supervisory fuzzy controller governs a sublevel fuzzy controller by altering its input normalization factors according to current level of ground motion. In order to simultaneously reduce the base displacement and superstructure responses of the base-isolated structure during seismic excitations, genetic algorithm is employed to optimize the supervisory fuzzy controller and the preload of piezoelectric friction damper. e efficiency of the proposed controller is also compared with passive controller and a linear quadratic Gauss optimal controller. Numerical results show that the proposed fuzzy logic controller has favorable performance in mitigating the responses of the base-isolated structure. 1. Introduction Base isolation has been demonstrated to be an effective technique that is used in seismic protection of crucial civil engineering structures. In order to mitigate the displacement of base-isolated structures, some designers usually installed dampers on isolation floor [1]. However, the performance of base-isolated structures against near-fault earthquakes has been questioned by several researchers [2, 3]. Near-fault earthquakes have the characteristic of long duration pulses with peak velocities in contrast to far-field earthquakes [4, 5]. Also, the long period of near-fault earthquakes coincides with the fundamental period of the base-isolated buildings [6, 7]. erefore, near-fault earthquakes possess much larger collapsing force for base-isolated structures than far-field earthquakes on account of resonance effect. Among the near- fault earthquakes in recent years, Chi-Chi earthquake has attracted an attention in the field of seismic engineering for its unique motion characteristics and great damage to civil engineering structures. is near-fault earthquake caused more than two thousand people deaths and wreaked havoc on the public property owing to the reverse oblique fractures in crustal rocks. During the Chi-Chi earthquake occurrence, scientists collected a large number of seismic records for different ground sites. Consequently, it is essential to design an appropriate control strategy to protect base- isolated structure under near-fault earthquakes for different ground sites. Although the supplement of dampers could reduce the damage of base-isolated systems against strong earthquake excitations, it may also abuse large damping forces and cause significant magnifications on the acceleration and interstory driſt of the base-isolated structure [8, 9]. Semiactive control is an intelligent control algorithm, which can regulate the output power of dampers according to current condition of structure responses. erefore, semiactive control has better adaptability than traditional passive control. Furthermore, semiactive control requires less power as compared to active control, which uses some powerful actuators to achieve ideal effects. For these reasons, many researchers have put forward all kinds of semiactive strategies for seismic protection. In these semiactive algorithms, fuzzy logic control has been a promising strategy, because it has the superiority in deal- ing with uncertain, complex, and nonlinear systems [10]. Hindawi Publishing Corporation Mathematical Problems in Engineering Volume 2015, Article ID 675698, 17 pages http://dx.doi.org/10.1155/2015/675698
Transcript

Research ArticleFuzzy Control for Seismic Protection of SemiactiveBase-Isolated Structures Subjected to Near-Fault Earthquakes

Dahai Zhao and Yongxing Li

School of Civil Engineering and Mechanics Yanshan University No 438 Hebei Road Qinhuangdao Hebei China

Correspondence should be addressed to Dahai Zhao zhaodhysueducn

Received 22 October 2015 Accepted 6 December 2015

Academic Editor Filippo Ubertini

Copyright copy 2015 D Zhao and Y Li This is an open access article distributed under the Creative Commons Attribution Licensewhich permits unrestricted use distribution and reproduction in any medium provided the original work is properly cited

This paper proposes a new fuzzy logic controller which is designed for seismic protection of base-isolated structures utilizingpiezoelectric friction damper against near-fault earthquakes for different ground sites According to the elastic design spectrumthat Eurocode 8 recommends one 5 damped elastic design spectrum for Chi-Chi earthquake is proposed to generate artificialearthquakes of different ground sitesThe proposed controller employs a hierarchic fuzzy control algorithm in which a supervisoryfuzzy controller governs a sublevel fuzzy controller by altering its input normalization factors according to current level of groundmotion In order to simultaneously reduce the base displacement and superstructure responses of the base-isolated structure duringseismic excitations genetic algorithm is employed to optimize the supervisory fuzzy controller and the preload of piezoelectricfriction damper The efficiency of the proposed controller is also compared with passive controller and a linear quadratic Gaussoptimal controller Numerical results show that the proposed fuzzy logic controller has favorable performance in mitigating theresponses of the base-isolated structure

1 Introduction

Base isolation has been demonstrated to be an effectivetechnique that is used in seismic protection of crucial civilengineering structures In order to mitigate the displacementof base-isolated structures some designers usually installeddampers on isolation floor [1] However the performanceof base-isolated structures against near-fault earthquakes hasbeen questioned by several researchers [2 3] Near-faultearthquakes have the characteristic of long duration pulseswith peak velocities in contrast to far-field earthquakes [4 5]Also the long period of near-fault earthquakes coincideswith the fundamental period of the base-isolated buildings[6 7] Therefore near-fault earthquakes possess much largercollapsing force for base-isolated structures than far-fieldearthquakes on account of resonance effect Among the near-fault earthquakes in recent years Chi-Chi earthquake hasattracted an attention in the field of seismic engineeringfor its unique motion characteristics and great damageto civil engineering structures This near-fault earthquakecaused more than two thousand people deaths and wreakedhavoc on the public property owing to the reverse oblique

fractures in crustal rocks During the Chi-Chi earthquakeoccurrence scientists collected a large number of seismicrecords for different ground sites Consequently it is essentialto design an appropriate control strategy to protect base-isolated structure under near-fault earthquakes for differentground sites

Although the supplement of dampers could reduce thedamage of base-isolated systems against strong earthquakeexcitations it may also abuse large damping forces and causesignificant magnifications on the acceleration and interstorydrift of the base-isolated structure [8 9] Semiactive controlis an intelligent control algorithm which can regulate theoutput power of dampers according to current condition ofstructure responses Therefore semiactive control has betteradaptability than traditional passive control Furthermoresemiactive control requires less power as compared to activecontrol which uses some powerful actuators to achieve idealeffects For these reasons many researchers have put forwardall kinds of semiactive strategies for seismic protection Inthese semiactive algorithms fuzzy logic control has been apromising strategy because it has the superiority in deal-ing with uncertain complex and nonlinear systems [10]

Hindawi Publishing CorporationMathematical Problems in EngineeringVolume 2015 Article ID 675698 17 pageshttpdxdoiorg1011552015675698

2 Mathematical Problems in Engineering

Constant acceleration

Constant displacement Constant velocity

S

Saag

25S

TB TC TD T (s)

Figure 1 Design spectrum envelope for Chi-Chi earthquake

Das et al [11] studied fuzzy control for seismic protectionof civil engineering structures using MR dampers Wangand Lee [12] used genetic algorithm to optimize fuzzy ruleto improve the performance of fuzzy control method Todeal with near-fault and far-field earthquake excitationsReigles and Symans [13] proposed a supervisory fuzzy con-troller to regulate two lower-level fuzzy controllers Kim andRoschke [14] proposed GA-fuzzy control method for smartbase-isolated benchmark building using supervisory controlmethod

In this study an improved fuzzy control is proposedfor seismic protection of base-isolated building with piezo-electric friction damper subjected to near-fault earthquakesof different ground sites According to the elastic designspectrum of the Eurocode 8 recommendation a 5 dampingratio elastic design spectrum for Chi-Chi earthquake is pro-posed to generate artificial earthquakes for different groundsites The proposed fuzzy controller employs a hierarchicfuzzy control algorithm which includes a supervisory fuzzycontroller and a sublevel fuzzy controller to alter its inputnormalization factors according to the current level of groundmotions The sublevel fuzzy control is to determine thecommand voltage of piezoelectric friction damper accordingto the velocity and displacement of the base isolation In orderto simultaneously reduce the base displacement and super-structure responses of the base-isolated structure geneticalgorithm is employed to optimize the supervisory fuzzycontrol and preload of piezoelectric friction damper Forcomparison the proposed fuzzy controller is also investigatedwith passive and linear quadratic Gauss optimal controllerA series of time history analyses of a base-isolated structureunder seismic excitations are also conducted to evaluate theperformance of the developed controller

2 Generate Artificial Earthquakes forDifferent Ground Sites

21 Elastic Design Spectrum for Chi-Chi Earthquake In orderto investigate the distinctive characteristics of near-fault

earthquakes some researchers have evaluated the perfor-mance of the near-fault earthquakes and proposed severaljudgment criterions Yang and Zhao [15] proposed a judg-ment for near-fault earthquakes The principles are listedas follows Firstly the ratio between PGV (Peak GroundVelocity) and PGA (Peak Ground Acceleration) is greaterthan 02 s Secondly the Joyner-Boore distance is between 0and 15 Km Thirdly the earthquake should possess obviouspulses with peak velocity Based on the above principles 29seismicwaves for Chi-Chi earthquake under different groundsites are selected from PEER database to generate elasticdesign spectrum In the late 1980s the European Committeefor Standardization released the first European code whichcontained structure design rules andminimum standards forearthquake resistant design With constant renovation forrecent years Eurocode 8 code includes detailed investigationand research on seismic design parameters of differentregions So this code has become the most authoritativeand influential standard in the world [16] According to theelastic design spectrum that Eurocode 8 code recommendsa 5 damping ratio elastic design spectrum for Chi-Chiearthquakes is proposed to generate artificial earthquakes fordifferent ground sites

The acceleration response spectral 119878119886(119879) as shown in

Figure 1 can be given as follows

119878119886(119879) = 119886

119892sdot 119878 sdot [1 +

119879

119879119861

(25 minus 1)] 0 le 119879 le 119879119861

119878119886(119879) = 119886

119892sdot 119878 sdot 25 119879

119861le 119879 le 119879

119862

119878119886(119879) = 119886

119892sdot 119878 sdot 25 sdot (

119879119862

119879)

120572

119879119862le 119879 le 119879

119863

119878119886(119879) = 119886

119892sdot 119878 sdot 25 sdot (

119879119862

119879)

120572

(119879119863

119879)

120573

119879119863le 119879

(1)

where 119886119892is the design PGA of Chi-Chi earthquake 119878 is the

amplification coefficient for different site conditions the cor-ner periods 119879

119861 119879119862 and 119879

119863represent constant acceleration

constant velocity and constant displacement spectral regionand 120572 and 120573 are dimensionless indexes respectively

Mathematical Problems in Engineering 3

Table 1 Selected Chi-Chi near-fault earthquakes

Earthquake Station 119881119904(ms) PGA (g) PGV (cms) PGD (cm) PGVPGA Joyner-Boore

distance (Km) Site classification

Chi-Chi

TCU110 21272 018061 52004 31216 029 1158

Soft soil

CHY101 25889 03829 9128 60731 024 994TCU123 27022 01468 375 3087 026 1491TCU051 35006 019428 42378 57953 022 764TCU060 37542 014895 41859 50693 029 851TCU101 38941 023429 56319 62133 025 211TCU056 4032 015539 38959 47705 026 1048

Medium soil

TCU104 41045 010059 43351 46291 044 1287CHY024 42773 022957 4642 42303 021 962TCU106 45137 015421 38177 30958 025 1497TCU053 45455 018717 43092 61802 023 595TCU054 46069 017207 45145 68386 027 528TCU136 4621 016921 48291 5337 029 827TCU082 47281 019836 51229 69534 026 516TCU063 47614 015751 63518 46961 041 978TCU049 48727 025431 5623 69733 023 376TCU068 48734 046625 25662 36592 056 04TCU116 49309 015476 42122 35828 028 1238TCU103 4941 015845 52488 50567 034 608TCU100 53513 011101 3915 4805 036 1137

Hard soil

TCU109 53513 015941 5711 37649 037 1306TCU087 53869 011697 4241 51865 037 698TCU050 54241 014417 37233 46979 026 949TCU048 55121 013435 42379 51429 032 1353TCU057 55523 011363 39208 51227 035 1183TCU075 57302 030134 79037 70594 027 089TCU052 5791 039658 11656 2212 043 03TCU128 59964 016034 63283 63457 040 1313TCU102 71427 026678 80098 75329 031 149

Table 2Variation of site factors andperiods forChi-Chi earthquakeunder different ground sites

Site 119881119904(ms) 119879

119861(s) 119879

119862(s) 119879

119863(s) 119878 (s) 120572 120573

Hard gt530 028 066 460 109 055 070Medium 390ndash530 040 096 580 113 082 020Soft lt390 060 160 640 116 110 100

As shown in Table 1 the selected seismic records areclassified into three categories which are hard medium andsoft soil site respectively The lower and upper limits foreach parameter of different site are listed in Table 2 Duringthe establishment of the design elastic spectrum the PGAis adjusted to 03 g The elastic design spectrum is obtainedby fitting the average response spectrum curve According tothese considerations the design response spectrum for Chi-Chi earthquake is shown in Figure 2 It can be seen from

the figures that the proposed design spectra are conservativecompared to the average spectrum Owing to the longduration pulses the corner periods are larger than that theEurocode 8 recommends

22 Artificial Earthquakes for Different Ground Sites Basedon the above discussions three artificial earthquakes thatare characterized by Chi-Chi near-fault earthquakes underdifferent ground sites are generated by power spectral densityfunction as shown in Figure 3 The artificial earthquakes arecalculated with a time step of 001 s and the PGA is equalto 03 g Artificial earthquakes for hard medium and softsoil site are shown in Figures 4ndash6 respectively From thesefigures it can be observed that the velocity time histories ofthe generated artificial earthquakes possess obvious pulseswith peak velocities Owing to the similar design spectrumthe time histories of the generated artificial for hard site andmedium site are the same despite several nuances However

4 Mathematical Problems in Engineering

0 2 4 6 8 1000

02

04

06

08

10Sp

ectr

al ac

cele

ratio

n (g

)

Period (s)

Design acceleration spectrumMean spectrum

(a) Hard soil site

0 2 4 6 8 1000

02

04

06

08

10

Spec

tral

acce

lera

tion

(g)

Period (s)

Design acceleration spectrumMean spectrum

(b) Medium soil site

0 2 4 6 8 1000

02

04

06

08

10

Spec

tral

acce

lera

tion

(g)

Period (s)

Design acceleration spectrumMean spectrum

(c) Soft soil site

Figure 2 Design spectrum envelopes for Chi-Chi earthquake

Time

d

I(t)

atb tdtc

b c

I(t) = (ttb)2

I(t) = e03(tc minus t)

Figure 3 Envelop for artificial earthquake

Mathematical Problems in Engineering 5

0 2 4 6 8 10 12 14 16 18 20

minus03

minus02

minus01

00

01

02

03

Acce

lera

tion

(g)

Time (s)

(a) Time history of acceleration

0 2 4 6 8 10 12 14 16 18 20

minus09

minus06

minus03

00

03

06

09

Velo

city

(ms

)

Time (s)

(b) Time history of velocity

Figure 4 Artificial earthquakes for hard soil site

0 2 4 6 8 10 12 14 16 18 20

minus03

minus02

minus01

00

01

02

03

Acce

lera

tion

(g)

Time (s)

(a) Time history of acceleration

0 2 4 6 8 10 12 14 16 18 20

minus09

minus06

minus03

00

03

06

09Ve

loci

ty (m

s)

Time (s)

(b) Time history of velocity

Figure 5 Artificial earthquake for medium soil site

0 2 4 6 8 10 12 14 16 18 20

minus03

minus02

minus01

00

01

02

03

Acce

lera

tion

(g)

Time (s)

(a) Time history of acceleration

0 2 4 6 8 10 12 14 16 18 20

minus09

minus06

minus03

00

03

06

09

Velo

city

(ms

)

Time (s)

(b) Time history of velocity

Figure 6 Artificial earthquake for soft soil site

6 Mathematical Problems in Engineering

the time history of the generated artificial earthquakes for softsoil is distinct with the other Particularly the peak velocityreaches 09ms which is significantly greater than the other

3 Model of Base-Isolated Structure andPiezoelectric Friction Damper

31 Equation of Motion for Base-Isolated Structure Consideran n-degree of freedom base-isolated structure with a piezo-electric friction damper at the isolation floor the dynamicequation of the base-isolated system is given by

MX (119905) + CX (119905) + KX (119905) = B119904U (119905) + E

119904119892(119905) (2)

where M C and K represent 119899 times 119899 mass damping andstiffness matrices respectively X(119905) X(119905) and X(119905) are theacceleration velocity and displacement vectors respectivelyU(119905) is the control force generated by the piezoelectric frictiondamper and

119892(119905) is the earthquake acceleration

Rewriting (2) in state-space form gives

Z (119905) = AZ (119905) + BU (119905) + E119892(119905) (3)

where

Z (119905) = [X (119905)X (119905)

]

E = [0119899times1

Mminus1E119904

]

B = [0119899times1

Mminus1B119904

]

A = [0119899times119899

I119899times119899

minusMminus1K minusMminus1C]

(4)

32 Model of Piezoelectric Friction Damper Piezoelectricfriction damper is a novel semiactive control device whichutilizes piezoelectric stacks to regulate the damping forceto provide a satisfying level of friction force Recently theauthors also proposed a piezoelectric friction damper andinvestigated their performances theoretically and experimen-tally [17]

During the movement of the base-isolated structure afriction damper has two possible motion states sticking andslipping phases [18 19] The friction force of the piezoelectricfriction damper is given as [20]

119873(119905) = 119873pre + 119862pz119881 (119905)

119891 (119905) = minus120583119873 (119905) sgn () = 0

minus120583119873 (119905) le 119891 (119905) le 120583119873 (119905) = 0

(5)

where 119873(119905) is the total contact force 119873pre represents thepreload of the piezoelectric friction damper 119862pz is thepiezoelectric coefficient of the piezoelectric actuator 119881(119905)is the input voltage of piezoelectric stack actuator 120583 is the

Table 3 Parameters of piezoelectric friction damper

Parameters Values120583 04119862pz 1125NV119881max 1000V

friction coefficient of the damper sgn(sdot) represents the signfunction related to the slip rate of the damper and 119891(119905)denotes damping force of piezoelectric friction damper

However the static state of the piezoelectric frictiondamper is complex to be estimated Shook et al [21] proposedan approximate calculation formula for the sticking frictionforce as given in the following

119891119904= minus120583119873 (119905) sgn ()

when 119891119904=1003816100381610038161003816119891119894 + 119891119903

1003816100381610038161003816 1003816100381610038161003816119891 (119905)

1003816100381610038161003816 ge 119891119904

119891119894= 119898119905119892= (119898

119887+

119899

sum

119894=1

119898119894) 119892

119891119903= 119896119887119909119887

(6)

where 119891119894is the inertial force applied on the mass 119891

119903is the

restoring force provided by the isolation bearing 119898119894is the

mass of the superstructure 119898119887and 119896

119887are the mass and

stiffness of base isolator and 119909119887is the displacement of base

isolatorThe parameters of piezoelectric friction damper are listed

in Table 3 And the preload of the piezoelectric frictiondamper can be optimized by genetic algorithm

4 GA-Based Hierarchic Fuzzy ControlAlgorithm

41 Framework of the Developed Fuzzy Logic Controller Thecontroller adopts a hierarchic fuzzy control algorithm inwhich a supervisory fuzzy controller governs a sublevelfuzzy controller by altering its input normalization factorsaccording to the current level of groundmotionThe sublevelfuzzy logic controller is designed to determine the commandvoltage of piezoelectric friction damper according to thevelocity and displacement of base isolation Piezoelectricfriction damper regulates the damping force according tothe input voltage Genetic algorithm is employed to optimizesupervisory fuzzy controller and preload of piezoelectricfriction damper according to an objective function and thegenerated artificial earthquakes for different ground sitesTheblock diagram of the system for the developed controller isshown in Figure 7

42 Sublevel Fuzzy Controller The sublevel fuzzy controlleris established in order to determine the command voltage ofthe piezoelectric friction damper The isolation displacementand velocity are selected as two input variables and commandvoltage is employed as a single output variable as shown inFigure 8The definitions of themembership function of input

Mathematical Problems in Engineering 7

Ground motion

Damping force

Semiactiveisolated

structure

Piezoelectricfriction damper

Ground velocity

Optimize

Voltage

Structural response

Isolation velocity and displacement

Sublevel fuzzycontroller

Supervisoryfuzzy controller

Optimize

Genetic algorithm

Nd

N

Figure 7 Block diagram of the base-isolated system for the fuzzy controller

minus10 minus05 00 05 100

1PL

PMPSZENSNM

Deg

ree o

f mem

bers

hip

Normalized displacement

NL

00 05 100

1PL

PMPSZENSNM

Deg

ree o

f mem

bers

hip

Normalized velocity

NL

0 200 400 600 800 10000

1VL

LMS

Deg

ree o

f mem

bers

hip

Voltage (V)

ZE

minus10 minus05

Figure 8 Input and output membership functions of sublevel fuzzy control

variables are as follows NL negative large NM negativemedium NS negative small ZE zero PS positive small PMpositive medium and PL positive large The definition ofthe membership function of output variable is as follows ZEzero S small M medium L large and VL very large Themembership functions are employed Gaussian type for inputand output variables The fuzzy control rules are defined inTable 4

In the establishment of fuzzy control rules it followsthe following principles if the isolation displacement andvelocity are in opposite sign then the output voltage becomessmall in order to ensure output small damping force inthe piezoelectric friction damper Contrarily if the isolationdisplacement and velocity have the same sign the outputvoltage becomes large Certainly when the displacement andvelocity are almost zero or small the command voltage is

8 Mathematical Problems in Engineering

Table 4 Fuzzy control rules adopted for sublevel fuzzy control

Velocity ofisolated floor

Displacement of isolated floorNL NM NS ZE PS PM PL

NL VL VL L L M S ZENM VL L L M S ZE SNS L L M S ZE S MZE L M S ZE S M LPS M S ZE S M L LPM S ZE S M L L VLPL ZE S M L L VL VL

minus1minus05

005

1

minus1minus05

005

1

500

1000

VelocityDisplacement

Volta

ge (V

)

Figure 9 Fuzzy control surface for sublevel fuzzy controller

about zero this means that piezoelectric friction damper actsas a passive friction damper The defuzzification of fuzzycontrol adopts the method of centroid to get a crisp outputvalue The control surface and color-filled contour line ofsublevel fuzzy control are depicted in Figure 9

43 Supervisory Fuzzy Logic Controller In the fuzzy logiccontrol normalization factors need to satisfy a certain objec-tive The oversize normalization factors can enlarge the basedisplacement effectively Contrarily too small normalizationfactors can result in large control force that amplifies theaccelerations of base-isolated structure Thus a supervisoryfuzzy logic control is proposed to adjust its normalizationfactors in real-time As discussed earlier near-fault earth-quakes usually have long duration pulses with peak velocitiesThus the supervisory fuzzy control employs ground velocityas single input variable to identify the characteristics ofthe ground motion The normalization factors of sublevelfuzzy control are selected as two output variables HereGaussian membership functions are used for input andoutput variables as shown in

120583gauss = exp[minus(119909 minus 119888)2

21205902] (7)

where 119888 and 120590 are the constant values that define the shape ofthe Gauss functions respectively

The rules of the supervisory fuzzy controller are definedby the following form

Rule119894 IF 119883 is 119860119894 then 1198841is 1198621198941 1198842is 1198621198942

119894 = 1 2 119872

(8)

where119872 is the number of fuzzy control rules 119883 is the inputvariable 119884

1and 119884

2are the output variables 119860119894 119862119894

1 and 119862119894

2

are the linguistic values characterized by input and outputmembership functions respectively One fuzzy control ruleis described by three Gaussian membership functions andeach membership function can be defined by two parameters(119888 and 120590) Therefore a total of five fuzzy control rules canbe optimized by encoding these two parameters into thegene using genetic algorithm Consequently a total of 30parameters are encoded into the chromosome to define theinference system of supervisory fuzzy controller as shown inFigure 10

Similar to normalization factors the preload of thepiezoelectric friction dampers has a great influence on thedamping effect Thus it is essential to establish an effectivesupervisory fuzzy logic controller and a suitable preloadof piezoelectric friction damper Generally for the seismicprotection of a base-isolated structure there is a trade-off between the isolation displacement and superstructureacceleration The main control objective is to depress theisolation displacementwithout excessively increasing acceler-ation response of the superstructure In this section a geneticalgorithm is employed to seek out an optimal solution forthe control of the base-isolated structure The flow chart ofgenetic algorithm is shown in Figure 11

Genetic algorithm is a computational model for thesimulation of Darwin natural genetic selection and biologicalevolution Different from the traditional search algorithmgenetic algorithm begins to search a group of optimal solu-tions from an initial random population by mutation andrecombination Each individual which consists of a set ofbinary strings is a solution to the objective problem Afterinitialization genetic algorithm uses a sort method to rankindividuals It compares each solution with other solutionsin the population to find whether it is dominated Duringthe process of creating a new generation it selects a suitableindividual according to the size of the fitness value Afterseveral generations the individual value gradually convergesto the best chromosome which is the optimal solution

The objective fitness function employed in this study isshown as follows

119869 = 06 times119910119887max

119910119887max

+ 04 timesradicsum119899

119894=1(119886119894max119886119894max)

2

119899 (9)

where 119910119887max and 119910119887max denote the peak base displacements

for the fuzzy control and uncontrolled cases respectively119886119894max and 119886119894max represent the peak superstructure accelera-tion for the fuzzy control and uncontrolled case respectively

The objective of genetic algorithm is tomake the objectivefitness function reach its minimum value by selecting oneset of parameters of supervisory fuzzy control and preload

Mathematical Problems in Engineering 9

0

1

X

0

1

Deg

ree o

f mem

bers

hip

Deg

ree o

f mem

bers

hip

0

1

Deg

ree o

f mem

bers

hip

1205901

1205901 1205902 1205903

Rule 1 (1 6) Rule 1 (7 12) Rule 5 (24 30)middot middot middot

c1

c1 c2 c3

1205902

Y1

1205903

Y2c2 c3

Figure 10 Encoding structure for genetic algorithm

of piezoelectric friction damper The initial population sizegenetic algebra and crossover probability are set to 20 50and 08 respectively Through inputting the artificial earth-quakes which are characterized by near-fault earthquakesfor different ground sites the supervisory fuzzy control andpreload of piezoelectric friction dampers can be optimizedThe fuzzy control surfaces of optimized supervisory fuzzycontrol are shown in Figure 12

5 Linear Quadratic Gaussian Controller

LQG (Linear Quadratic Gaussian) method is based onKalman filter technique which has become a widely usedcontrol algorithm For comparison purpose LQG is adoptedto regulate the contact normal force of piezoelectric frictiondamper in the study The optimal controller takes groundacceleration as white noise and considers the velocity anddisplacement of base isolation as feedback signals Thecontrol performance index is defined as follows [22]

119869 = lim120591rarr+infin

1

120591

sdot 119864 int

120591

0

[Z (119905)119879QZ (119905) + U (119905)119879RU (119905)] 119889 (119905) (10)

where Q2119899times2119899

and R1times1

are semi-positive definite matrix andpositive definite matrix respectivelyThe control force can beobtained as follows

U (119905) = minusGZ (119905) (11)

G = Rminus1B119879P (12)

where P can be computed by the solution of the Riccatiequation as follows

minusPA minus A119879P + PBRminus1B119879P minusQ = 0 (13)

The control force obtained from the above equation isactive control force which could not be always achieved bypiezoelectric friction damper It is realized that the directionof active control force is opposite to the slipping direction ofpiezoelectric friction damper Therefore the desired controlforce119906

119889(119905) can be achieved according to the following criteria

119906119889(119905)

=

119891max sgn (119887) (119906active

119887lt 0

10038161003816100381610038161003816119906active10038161003816100381610038161003816 gt 119891max)

10038161003816100381610038161003816119906active10038161003816100381610038161003816 sgn (119887) (119906

active119887lt 0

10038161003816100381610038161003816119906active10038161003816100381610038161003816 le 119891max)

119891min sgn (119887) (119906active

119887ge 0)

(14)

10 Mathematical Problems in Engineering

Table 5 Parameters of base-isolated structure

Floor masses(kg)

Stiffness values(kNm)

Dampingcoefficients(kN sm)

Isolated floor 6800 232 745First floor 5897 33732 67Second floor 5897 29093 58Third floor 5897 28621 57Fourth floor 5897 24954 50Fifth floor 5897 19059 38

No

Yes

Encode

Generate initial random population

Calculate the value of fitness and rank

Copy crossover and mutation

Decode

Optimal solution

Whether or not to meet thecondition of convergence

Figure 11 Flow chart of genetic algorithm

where 119906active is the control force obtained from LQG con-troller

119887is the velocity of base isolator119891max and119891min are the

maximum and minimum friction forces of the piezoelectricfriction damper respectively

6 Numerical Simulations

61 Model of the Base-Isolated Structure A five-story base-isolated building which is proposed by He et al is employedto evaluate the performance of developed fuzzy controllers[18] The fundamental period of the five-story building is03 s For the given isolation parameters the fundamentalperiod of the base-isolated building becomes 25 sThereforean isolation ratio 120575 equal to 83 (=2503) is obtainedThe model of the base-isolated structure with piezoelectricfriction damper is shown in Figure 13 The parameters of thebase-isolated structure are shown in Table 5

62 Performance Evaluation Index In order to evaluate theperformance of base-isolated structure for different controlalgorithms a total of nine performance indexes are employedin this study [23] as shown in Table 6

The performance indexes J1through J

5denote the struc-

ture responses for the controlled building normalized byuncontrolled structure respectively The performance indexJ6evaluates the peak control force normalized by the peak

base shear for controlled structure The performance indexesJ7and J8represent RMS (Root Mean Square) base displace-

ments and RMS floor accelerations respectively J9computes

the energy dissipated by friction dampers normalized by theearthquake input energy to the controlled structure

63 Simulation Results and Analysis A total of nine seis-mic excitations that contain six real ground motions andthree artificial earthquakes are selected to evaluate the per-formance of the optimized fuzzy logic controller In thisstudy the time histories of strong earthquake which rangefrom 20 s to 70 s are selected for numerical simulation andanalysis

The numerical results for various earthquakes are listedin Table 7 In the table the Genetic Algorithm HierarchicFuzzy Logic Control is named as GHFLC Moreover forcomparison purpose the results for an optimal controller andpassive operation of friction damper are also listed in thetable Numbers in bold font indicate the best results amongall control cases

Base displacement is an important index to evaluatethe effectiveness for different controllers For a base-isolatedstructure the reduction of base displacement is a primarypurpose to prevent permanent damage for isolation bearingsor adjacent buildings Although passive operation of frictiondampers can successfully reduce the performance indexassociated with the peak and RMS base displacements (J

3and

J7) it causes significant amplification in peak and RMS floor

accelerations (J5and J

8) for most cases due to the passive

control For example as compared to the uncontrolledstructure for TCU052 TCU053 and TCU054 earthquakespassive control leads to 6 45 and 42 amplification inpeak floor acceleration respectively However the proposedfuzzy controller can successfully improve the base-isolatedstructure acceleration at the cost of slight deterioration in theperformance indices J

3and J7on comparison with passive

control For example for TCU052 TCU053 and TCU054earthquakes GHFLC results in 15 13 and 16 decrease inpeak floor accelerations respectively As compared to passivecontrol there are 9 3 and 7 increase in peak basedisplacements

The time histories of friction force and force-displacement curves of friction dampers for differentcontrollers subjected to TCU052 earthquake are shown inFigure 14 From the figures it can be seen that the passivecontrol outputs lager damper force than GHFLC Becausethe supervisory fuzzy control can alter input normalizationfactors of sublevel FLC according to the current level ofground motion there are some serrations presented at theedge of the hysteretic curve of piezoelectric friction damper

The comparison of the performance indexes J3 J7 J5and

J8under different control cases is shown in Figures 15 and

16 respectively From these figures it can be seen that thefuzzy controller is more effective than passive and optimal

Mathematical Problems in Engineering 11O

utpu

t

009

055

026

000033

000094000

Input ground velocity (ms)

Nd

N

(a) Hard soilO

utpu

t

Input ground velocity (ms)

071

042

000

008000

037

103000

Nd

N

(b) Medium soil

Out

put

Input ground velocity (ms)

107

053

000045

011000

117000

Nd

N

(c) Soft soil

Figure 12 Control surface for optimized supervisory fuzzy control

PFD

Fixed reference

LRB

Figure 13 Model of the base-isolated structure

12 Mathematical Problems in Engineering

Table 6 Performance index

Peak base shear Peak interstory drift RMS base displacement

1198691=max119905

10038171003817100381710038171198810 (119905)1003817100381710038171003817

max119905

100381710038171003817100381710038171198810(119905)10038171003817100381710038171003817

1198694=

max119905119891

10038171003817100381710038171003817119889119891(119905)10038171003817100381710038171003817

max119905119891

10038171003817100381710038171003817119889119891(119905)10038171003817100381710038171003817

1198697=

max119894

1003817100381710038171003817120590119889 (119905)1003817100381710038171003817

max119905

1003817100381710038171003817119889 (119905)1003817100381710038171003817

Peak structural shear Peak floor acceleration RMS floor acceleration

1198692=max119905

10038171003817100381710038171198811 (119905)1003817100381710038171003817

max119905

100381710038171003817100381710038171198811(119905)10038171003817100381710038171003817

1198695=

max119905119891

10038171003817100381710038171003817119886119891(119905)10038171003817100381710038171003817

max119905119891

10038171003817100381710038171003817119886119891(119905)10038171003817100381710038171003817

1198698=max119891

1003817100381710038171003817120590119886 (119905)1003817100381710038171003817

max119891

1003817100381710038171003817119886 (119905)1003817100381710038171003817

Peak base displacement Peak control force Energy dissipated by PFD

1198693=max119905

1003817100381710038171003817119909119887 (119905)1003817100381710038171003817

max119905

1003817100381710038171003817119909119887 (119905)1003817100381710038171003817

1198696=max119905

1003817100381710038171003817119891119889 (119905)1003817100381710038171003817

max119905

10038171003817100381710038171198810 (119905)1003817100381710038171003817

1198699=

int119879

0

119891119889(119905) 119887(119905) 119889119905

int119879

0

1198810(119905) 119892(119905) 119889119905

Table 7 Results of numerical simulation

Earthquake Control case 1198691

1198692

1198693

1198694

1198695

1198696

1198697

1198698

1198699

TCU102(hard site)

Passive 081 082 068 085 094 048 057 082 078Optimal 092 095 075 099 087 043 068 081 069GHFLC 087 091 071 093 082 041 061 078 073

TCU052(hard site)

Passive 079 079 046 082 106 036 038 089 087Optimal 087 087 057 087 098 029 049 085 079GHFLC 083 082 055 082 091 033 044 079 084

Artificialearthquake(hard site)

Passive 072 074 054 076 092 054 049 090 084Optimal 084 086 069 083 089 047 057 086 073GHFLC 076 077 061 079 083 042 052 081 076

TCU053(medium site)

Passive 061 065 039 071 145 032 037 116 089Optimal 069 072 046 076 136 031 045 117 078GHFLC 062 062 042 065 132 026 044 109 072

TCU054(medium site)

Passive 071 073 043 073 142 084 038 121 088Optimal 081 087 045 085 132 079 052 125 086GHFLC 075 071 040 074 126 082 045 113 076

Artificialearthquake(medium site)

Passive 054 057 038 064 123 067 036 117 091Optimal 067 066 047 067 119 078 048 113 079GHFLC 058 061 040 062 113 072 041 109 085

TCU110(soft soil site)

Passive 077 078 047 077 103 050 045 089 095Optimal 083 082 052 085 107 046 052 099 087GHFLC 086 086 056 086 104 042 049 093 090

CHY101(soft soil site)

Passive 069 071 058 075 086 066 054 092 084Optimal 075 073 062 074 087 064 055 088 079GHFLC 063 067 054 067 079 065 051 087 083

Artificialearthquake(soft site)

Passive 057 064 061 068 097 061 058 098 088Optimal 071 070 074 075 094 058 071 093 083GHFLC 065 062 067 069 085 055 063 086 076

controller in simultaneously depressing the superstructureacceleration and base displacement For example the appli-cation of developed fuzzy controller leads to an average of112 decrease in peak floor acceleration and an average ofonly 36 increase in peak base displacement as compared topassive control Particularly optimal controller produces anaverage of only 41 reduction in peak floor acceleration and

leads to 79 increase in peak base displacement as comparedto passive control Therefore the improved fuzzy controlmethod shows better performance than passive and optimalcontrol

In order to further evaluate the performance of differentcontrollers the energy time histories for different controllersare compared with each other For a base-isolated structure

Mathematical Problems in Engineering 13

20 30 40 50 60 70minus20

minus10

00

10

20Fr

ictio

n fo

rce (

kN)

Time (s)minus03 minus02 minus01 00 01 02 03

minus20

minus10

00

10

20

Fric

tion

forc

e (kN

)

Displacement (m)

(a) Passive control

20 30 40 50 60 70minus20

minus10

00

10

20

Fric

tion

forc

e (kN

)

Time (s)minus03 minus02 minus01 00 01 02 03

minus20

minus10

00

10

20

Fric

tion

forc

e (kN

)

Displacement (m)

(b) GHFLC method

Figure 14 Time histories of friction force and force-displacement diagram against TCU052 earthquake

1 2 3 4 5 6 7 8 903

04

05

06

07

08

Excitation case

Passive OptimalGHFLC

1 2 3 4 5 6 7 8 903

04

05

06

07

Excitation casePassive

GHFLC Optimal

J 3 J 5

Figure 15 Comparisons on the performance indexes J3and J7for different control cases

14 Mathematical Problems in Engineering

1 2 3 4 5 6 7 8 907

08

09

10

11

12

13

14

15

Excitation casePassive

GHFLC Optimal

1 2 3 4 5 6 7 8 907

08

09

10

11

12

13

Excitation case

Passive

GHFLC Optimal

J 8J 5

Figure 16 Comparison of the performance indexes J5and J8for different control cases

with piezoelectric friction dampers installed on the isolationthe energy equations are defined as follows

119864119870+ 119864120585+ 119864119878+ 119864119867= 119864119868

119864119870=1

2119879

119905119872119905

119864120585= int

119905

0

119879

119888 119889119905

119864119878= int

119905

0

119909119879

119870119889119909

119864119867= minusint

119905

0

119906119879

119864119879

119904119889119909

119864119868= minusint

119905

0

gMI 119889119909

(15)

where 119864119870 119864120585 119864119878 119864119867 and 119864

119868denote the absolute kinetic

energy damping energy elastic strain energy energy dis-sipated by piezoelectric friction dampers and total inputenergy respectively The energy time histories for differentcontrollers against TCU052Chi-Chi earthquake are shown inFigure 17 It can be seen from the figures that the piezoelectricfriction dampers dissipate most of the input energy fordifferent control cases subjected to TCU052 earthquake

In order to compare different effects under near-faultground motions recorded for different sites the average ofinput energy and structure responses subjected to near-faultearthquakes are given in Table 8

As shown in Table 8 the near-fault earthquakes forsoft sites are more destructive than hard sites For instancecompared to hard sites the input energy and the base dis-placement of RMS of the base-isolated structure for soft soil

increase by 143 and 256 respectively However GHFLCpossesses favorable performance under different ground sitesand the damping effect has no distinctly direct relationshipwith site category

As discussed in Section 61 the isolation ratio of thesimulation model equals 83 In order to evaluate the effectsof isolation ratio on the damping performance of GHFLC thestiffness value of isolation is adjusted to 1045 and 452 kNmrespectively Then the numerical results for different valuesof isolation ratio (120575 = 4 6) are obtained The performanceindexes J

3and J5for different isolation ratios are shown in

Figures 18 and 19 respectivelyFor base-isolated structure isolation ratio has a signifi-

cant influence on the isolation effect A larger isolation ratiowhich means a minor stiffness value of isolation usuallyleads to conspicuous enlargement of base displacement anddecrease of superstructural responses due to the increaseof fundamental vibration period and vice versa Howeveras shown in Figures 18 and 19 the shock absorption rateof GHFLC has little change when isolation ratio variesdifferently and the proposed fuzzy control shows favorableeffectiveness in the diverse isolation ratios of base-isolatedstructures

7 Conclusions

In this study an optimized fuzzy logic control which isdesigned for Chi-Chi near-fault earthquakes under differentground sites is proposed An elastic design spectrum isproposed to generate near-fault earthquakes for differentground sitesThe characteristic of the design spectrum is thatit has larger periods and peak acceleration than conventionalspectrum Genetic algorithm is employed to optimize thesupervisory fuzzy controller and preload of piezoelectric

Mathematical Problems in Engineering 15

Table 8 Average ofinput energy and structure responses subjected to near-fault earthquakes

Site classification Input energy (kNsdotm) Base shear (kN) Base displacement ofRMS (m)

Structure accelerationof RMS (g)

Hard soil 24375 475 0047 0432Medium soil 26746 498 0054 0476Soft soil 27857 568 0059 0531

20 30 40 50 60 7000

05

10

15

20

25

Input energyEnergy dissipated by dampers

Time (s)

Ener

gy (k

Nmiddotm

)

times104

(a) Passive control

20 30 40 50 60 7000

05

10

15

20

25

30

Time (s)

Input energyEnergy dissipated by dampers

Ener

gy (k

Nmiddotm

)

times104

(b) Optimal control

20 30 40 50 60 7000

05

10

15

20

25

30

Input energyEnergy dissipated by dampers

Time (s)

Ener

gy (k

Nmiddotm

)

times104

(c) GHFLC method

Figure 17 Energy time histories subjected to Chi-Chi TCU052 earthquake

friction dampers according to three artificial earthquakesthat are characterized by Chi-Chi earthquakes Passive andoptimal controllers are also compared with the performanceof the developed fuzzy controller The simulation resultsreveal that the developed semiactive fuzzy controller hasbetter performance than traditional passive and optimal con-troller in simultaneously reducing the base displacement and

floor acceleration under near-fault earthquakes for differentground sites

Conflict of Interests

The authors declare no conflict of interests regarding thepublication of this paper

16 Mathematical Problems in Engineering

1 2 3 4 5 6 7 8 903

04

05

06

07

08

Excitation casePassive

GHFLC Optimal

1 2 3 4 5 6 7 8 907

08

09

10

11

12

13

14

15

Excitation case

Passive

GHFLC Optimal

J 3 J 5Figure 18 Comparisons on the performance indexes J

3and J5for different control cases (120575 = 4)

1 2 3 4 5 6 7 8 903

04

05

06

07

08

Excitation casePassive

GHFLC Optimal

1 2 3 4 5 6 7 8 907

08

09

10

11

12

13

14

15

Excitation casePassive

GHFLC Optimal

J 3 J 5

Figure 19 Comparisons on the performance indexes J3and J5for different control cases (120575 = 6)

Acknowledgments

This research was supported by National Natural ScienceFoundation of China under Grant no 51308487 no 41402261and no 51408526 Hebei Provincial Natural Science Founda-tion ofChina underGrant no E2014203055 and the ExcellentYouth Foundation of Hebei Educational Committee underGrant no YQ2013015 The support for this research is greatlyappreciated

References

[1] C Alhan and H Gavin ldquoA parametric study of linear and non-linear passively damped seismic isolation systems for buildingsrdquoEngineering Structures vol 26 no 4 pp 485ndash497 2004

[2] R S Jangid and J M Kelly ldquoBase isolation for near-faultmotionsrdquoEarthquake Engineering and Structural Dynamics vol30 no 5 pp 691ndash707 2001

[3] J Shen M-H Tsai K-C Chang and G C Lee ldquoPerformanceof a seismically isolated bridge under near-fault earthquake

Mathematical Problems in Engineering 17

ground motionsrdquo Journal of Structural Engineering vol 130 no6 pp 861ndash868 2004

[4] F Mazza A Vulcano and M Mazza ldquoNonlinear dynamicresponse of RC buildings with different base Isolation systemssubjected to horizontal and vertical components of near-faultground motionsrdquo Open Construction and Building TechnologyJournal vol 6 pp 373ndash383 2012

[5] F Mazza and A Vulcano ldquoEffects of near-fault ground motionson the nonlinear dynamic response of base-isolated rc framedbuildingsrdquo Earthquake Engineering and Structural Dynamicsvol 41 no 2 pp 211ndash232 2012

[6] O E Ozbulut and S Hurlebaus ldquoFuzzy control of piezoelectricfriction dampers for seismic protection of smart base isolatedbuildingsrdquo Bulletin of Earthquake Engineering vol 8 no 6 pp1435ndash1455 2010

[7] O E Ozbulut M Bitaraf and S Hurlebaus ldquoAdaptive controlof base-isolated structures against near-field earthquakes usingvariable friction dampersrdquo Engineering Structures vol 33 no12 pp 3143ndash3154 2011

[8] J M Kelly ldquoThe role of damping in seismic isolationrdquo Earth-quake Engineering and Structural Dynamics vol 28 no 1 pp3ndash20 1999

[9] F Mazza and A Vulcano ldquoNonlinear response of RC framedbuildings with isolation and supplemental damping at the basesubjected to near-fault earthquakesrdquo Journal of EarthquakeEngineering vol 13 no 5 pp 690ndash715 2009

[10] M Bitaraf and S Hurlebaus ldquoSemi-active adaptive control ofseismically excited 20-story nonlinear buildingrdquo EngineeringStructures vol 56 no 11 pp 2107ndash2118 2013

[11] D Das T K Datta and A Madan ldquoSemiactive fuzzy controlof the seismic response of building frames with MR dampersrdquoEarthquake Engineering and Structural Dynamics vol 41 no 1pp 99ndash118 2012

[12] A-P Wang and C-D Lee ldquoFuzzy sliding mode control for abuilding structure based on genetic algorithmsrdquo EarthquakeEngineering and Structural Dynamics vol 31 no 4 pp 881ndash8952002

[13] D G Reigles and M D Symans ldquoSupervisory fuzzy controlof a base-isolated benchmark building utilizing a neuro-fuzzymodel of controllable fluid viscous dampersrdquo Structural Controland Health Monitoring vol 13 no 2-3 pp 724ndash747 2006

[14] H-S Kim and P N Roschke ldquoGA-fuzzy control of smartbase isolated benchmark building using supervisory controltechniquerdquo Advances in Engineering Software vol 38 no 7 pp453ndash465 2007

[15] D Yang and Y Zhao ldquoEffects of rupture forward directivity andfling step of near-fault groundmotions on seismic performanceof base-isolated building structurerdquo Acta Seismologica Sinicavol 32 no 5 pp 579ndash587 2010

[16] Y E-A Mohamedzein J A Abdalla and A Abdelwahab ldquoSiteresponse and earthquake design spectra for central KhartoumSudanrdquoBulletin of Earthquake Engineering vol 4 no 3 pp 277ndash293 2006

[17] D Zhao and H Li ldquoShaking table tests and analyses of semi-active fuzzy control for structural seismic reduction with apiezoelectric variable-friction damperrdquo Smart Materials andStructures vol 19 no 10 Article ID 105031 2010

[18] W L He A K Agrawal and J N Yang ldquoNovel semiactivefriction controller for linear structures against earthquakesrdquoJournal of Structural Engineering vol 129 no 7 pp 941ndash9502003

[19] J N Yang and A K Agrawal ldquoSemi-active hybrid controlsystems for nonlinear buildings against near-field earthquakesrdquoEngineering Structures vol 24 no 3 pp 271ndash280 2002

[20] O E Ozbulut and S Hurlebaus ldquoOptimal design of supere-lastic-friction base isolators for seismic protection of highwaybridges against near-field earthquakesrdquo Earthquake Engineeringand Structural Dynamics vol 40 no 3 pp 273ndash291 2011

[21] D A Shook P N Roschke and O E Ozbulut ldquoSuperelasticsemi-active damping of a base-isolated structurerdquo StructuralControl and HealthMonitoring vol 15 no 5 pp 746ndash768 2008

[22] K D PhamG JinM K Sain B F Spencer Jr and S R LibertyldquoGeneralized linear quadratic Gaussian techniques for the windbenchmark problemrdquo Journal of Engineering Mechanics vol130 no 4 pp 466ndash470 2004

[23] S Nagarajaiah and S Narasimhan ldquoSmart base-isolated bench-mark building Part II Phase I sample controllers for linearisolation systemsrdquo Structural Control and Health Monitoringvol 13 no 2-3 pp 605ndash625 2006

Submit your manuscripts athttpwwwhindawicom

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

MathematicsJournal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Mathematical Problems in Engineering

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Differential EquationsInternational Journal of

Volume 2014

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Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

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Complex AnalysisJournal of

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CombinatoricsHindawi Publishing Corporationhttpwwwhindawicom Volume 2014

International Journal of

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Journal of

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Function Spaces

Abstract and Applied AnalysisHindawi Publishing Corporationhttpwwwhindawicom Volume 2014

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Discrete Dynamics in Nature and Society

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Decision SciencesAdvances in

Discrete MathematicsJournal of

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Volume 2014 Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Stochastic AnalysisInternational Journal of

2 Mathematical Problems in Engineering

Constant acceleration

Constant displacement Constant velocity

S

Saag

25S

TB TC TD T (s)

Figure 1 Design spectrum envelope for Chi-Chi earthquake

Das et al [11] studied fuzzy control for seismic protectionof civil engineering structures using MR dampers Wangand Lee [12] used genetic algorithm to optimize fuzzy ruleto improve the performance of fuzzy control method Todeal with near-fault and far-field earthquake excitationsReigles and Symans [13] proposed a supervisory fuzzy con-troller to regulate two lower-level fuzzy controllers Kim andRoschke [14] proposed GA-fuzzy control method for smartbase-isolated benchmark building using supervisory controlmethod

In this study an improved fuzzy control is proposedfor seismic protection of base-isolated building with piezo-electric friction damper subjected to near-fault earthquakesof different ground sites According to the elastic designspectrum of the Eurocode 8 recommendation a 5 dampingratio elastic design spectrum for Chi-Chi earthquake is pro-posed to generate artificial earthquakes for different groundsites The proposed fuzzy controller employs a hierarchicfuzzy control algorithm which includes a supervisory fuzzycontroller and a sublevel fuzzy controller to alter its inputnormalization factors according to the current level of groundmotions The sublevel fuzzy control is to determine thecommand voltage of piezoelectric friction damper accordingto the velocity and displacement of the base isolation In orderto simultaneously reduce the base displacement and super-structure responses of the base-isolated structure geneticalgorithm is employed to optimize the supervisory fuzzycontrol and preload of piezoelectric friction damper Forcomparison the proposed fuzzy controller is also investigatedwith passive and linear quadratic Gauss optimal controllerA series of time history analyses of a base-isolated structureunder seismic excitations are also conducted to evaluate theperformance of the developed controller

2 Generate Artificial Earthquakes forDifferent Ground Sites

21 Elastic Design Spectrum for Chi-Chi Earthquake In orderto investigate the distinctive characteristics of near-fault

earthquakes some researchers have evaluated the perfor-mance of the near-fault earthquakes and proposed severaljudgment criterions Yang and Zhao [15] proposed a judg-ment for near-fault earthquakes The principles are listedas follows Firstly the ratio between PGV (Peak GroundVelocity) and PGA (Peak Ground Acceleration) is greaterthan 02 s Secondly the Joyner-Boore distance is between 0and 15 Km Thirdly the earthquake should possess obviouspulses with peak velocity Based on the above principles 29seismicwaves for Chi-Chi earthquake under different groundsites are selected from PEER database to generate elasticdesign spectrum In the late 1980s the European Committeefor Standardization released the first European code whichcontained structure design rules andminimum standards forearthquake resistant design With constant renovation forrecent years Eurocode 8 code includes detailed investigationand research on seismic design parameters of differentregions So this code has become the most authoritativeand influential standard in the world [16] According to theelastic design spectrum that Eurocode 8 code recommendsa 5 damping ratio elastic design spectrum for Chi-Chiearthquakes is proposed to generate artificial earthquakes fordifferent ground sites

The acceleration response spectral 119878119886(119879) as shown in

Figure 1 can be given as follows

119878119886(119879) = 119886

119892sdot 119878 sdot [1 +

119879

119879119861

(25 minus 1)] 0 le 119879 le 119879119861

119878119886(119879) = 119886

119892sdot 119878 sdot 25 119879

119861le 119879 le 119879

119862

119878119886(119879) = 119886

119892sdot 119878 sdot 25 sdot (

119879119862

119879)

120572

119879119862le 119879 le 119879

119863

119878119886(119879) = 119886

119892sdot 119878 sdot 25 sdot (

119879119862

119879)

120572

(119879119863

119879)

120573

119879119863le 119879

(1)

where 119886119892is the design PGA of Chi-Chi earthquake 119878 is the

amplification coefficient for different site conditions the cor-ner periods 119879

119861 119879119862 and 119879

119863represent constant acceleration

constant velocity and constant displacement spectral regionand 120572 and 120573 are dimensionless indexes respectively

Mathematical Problems in Engineering 3

Table 1 Selected Chi-Chi near-fault earthquakes

Earthquake Station 119881119904(ms) PGA (g) PGV (cms) PGD (cm) PGVPGA Joyner-Boore

distance (Km) Site classification

Chi-Chi

TCU110 21272 018061 52004 31216 029 1158

Soft soil

CHY101 25889 03829 9128 60731 024 994TCU123 27022 01468 375 3087 026 1491TCU051 35006 019428 42378 57953 022 764TCU060 37542 014895 41859 50693 029 851TCU101 38941 023429 56319 62133 025 211TCU056 4032 015539 38959 47705 026 1048

Medium soil

TCU104 41045 010059 43351 46291 044 1287CHY024 42773 022957 4642 42303 021 962TCU106 45137 015421 38177 30958 025 1497TCU053 45455 018717 43092 61802 023 595TCU054 46069 017207 45145 68386 027 528TCU136 4621 016921 48291 5337 029 827TCU082 47281 019836 51229 69534 026 516TCU063 47614 015751 63518 46961 041 978TCU049 48727 025431 5623 69733 023 376TCU068 48734 046625 25662 36592 056 04TCU116 49309 015476 42122 35828 028 1238TCU103 4941 015845 52488 50567 034 608TCU100 53513 011101 3915 4805 036 1137

Hard soil

TCU109 53513 015941 5711 37649 037 1306TCU087 53869 011697 4241 51865 037 698TCU050 54241 014417 37233 46979 026 949TCU048 55121 013435 42379 51429 032 1353TCU057 55523 011363 39208 51227 035 1183TCU075 57302 030134 79037 70594 027 089TCU052 5791 039658 11656 2212 043 03TCU128 59964 016034 63283 63457 040 1313TCU102 71427 026678 80098 75329 031 149

Table 2Variation of site factors andperiods forChi-Chi earthquakeunder different ground sites

Site 119881119904(ms) 119879

119861(s) 119879

119862(s) 119879

119863(s) 119878 (s) 120572 120573

Hard gt530 028 066 460 109 055 070Medium 390ndash530 040 096 580 113 082 020Soft lt390 060 160 640 116 110 100

As shown in Table 1 the selected seismic records areclassified into three categories which are hard medium andsoft soil site respectively The lower and upper limits foreach parameter of different site are listed in Table 2 Duringthe establishment of the design elastic spectrum the PGAis adjusted to 03 g The elastic design spectrum is obtainedby fitting the average response spectrum curve According tothese considerations the design response spectrum for Chi-Chi earthquake is shown in Figure 2 It can be seen from

the figures that the proposed design spectra are conservativecompared to the average spectrum Owing to the longduration pulses the corner periods are larger than that theEurocode 8 recommends

22 Artificial Earthquakes for Different Ground Sites Basedon the above discussions three artificial earthquakes thatare characterized by Chi-Chi near-fault earthquakes underdifferent ground sites are generated by power spectral densityfunction as shown in Figure 3 The artificial earthquakes arecalculated with a time step of 001 s and the PGA is equalto 03 g Artificial earthquakes for hard medium and softsoil site are shown in Figures 4ndash6 respectively From thesefigures it can be observed that the velocity time histories ofthe generated artificial earthquakes possess obvious pulseswith peak velocities Owing to the similar design spectrumthe time histories of the generated artificial for hard site andmedium site are the same despite several nuances However

4 Mathematical Problems in Engineering

0 2 4 6 8 1000

02

04

06

08

10Sp

ectr

al ac

cele

ratio

n (g

)

Period (s)

Design acceleration spectrumMean spectrum

(a) Hard soil site

0 2 4 6 8 1000

02

04

06

08

10

Spec

tral

acce

lera

tion

(g)

Period (s)

Design acceleration spectrumMean spectrum

(b) Medium soil site

0 2 4 6 8 1000

02

04

06

08

10

Spec

tral

acce

lera

tion

(g)

Period (s)

Design acceleration spectrumMean spectrum

(c) Soft soil site

Figure 2 Design spectrum envelopes for Chi-Chi earthquake

Time

d

I(t)

atb tdtc

b c

I(t) = (ttb)2

I(t) = e03(tc minus t)

Figure 3 Envelop for artificial earthquake

Mathematical Problems in Engineering 5

0 2 4 6 8 10 12 14 16 18 20

minus03

minus02

minus01

00

01

02

03

Acce

lera

tion

(g)

Time (s)

(a) Time history of acceleration

0 2 4 6 8 10 12 14 16 18 20

minus09

minus06

minus03

00

03

06

09

Velo

city

(ms

)

Time (s)

(b) Time history of velocity

Figure 4 Artificial earthquakes for hard soil site

0 2 4 6 8 10 12 14 16 18 20

minus03

minus02

minus01

00

01

02

03

Acce

lera

tion

(g)

Time (s)

(a) Time history of acceleration

0 2 4 6 8 10 12 14 16 18 20

minus09

minus06

minus03

00

03

06

09Ve

loci

ty (m

s)

Time (s)

(b) Time history of velocity

Figure 5 Artificial earthquake for medium soil site

0 2 4 6 8 10 12 14 16 18 20

minus03

minus02

minus01

00

01

02

03

Acce

lera

tion

(g)

Time (s)

(a) Time history of acceleration

0 2 4 6 8 10 12 14 16 18 20

minus09

minus06

minus03

00

03

06

09

Velo

city

(ms

)

Time (s)

(b) Time history of velocity

Figure 6 Artificial earthquake for soft soil site

6 Mathematical Problems in Engineering

the time history of the generated artificial earthquakes for softsoil is distinct with the other Particularly the peak velocityreaches 09ms which is significantly greater than the other

3 Model of Base-Isolated Structure andPiezoelectric Friction Damper

31 Equation of Motion for Base-Isolated Structure Consideran n-degree of freedom base-isolated structure with a piezo-electric friction damper at the isolation floor the dynamicequation of the base-isolated system is given by

MX (119905) + CX (119905) + KX (119905) = B119904U (119905) + E

119904119892(119905) (2)

where M C and K represent 119899 times 119899 mass damping andstiffness matrices respectively X(119905) X(119905) and X(119905) are theacceleration velocity and displacement vectors respectivelyU(119905) is the control force generated by the piezoelectric frictiondamper and

119892(119905) is the earthquake acceleration

Rewriting (2) in state-space form gives

Z (119905) = AZ (119905) + BU (119905) + E119892(119905) (3)

where

Z (119905) = [X (119905)X (119905)

]

E = [0119899times1

Mminus1E119904

]

B = [0119899times1

Mminus1B119904

]

A = [0119899times119899

I119899times119899

minusMminus1K minusMminus1C]

(4)

32 Model of Piezoelectric Friction Damper Piezoelectricfriction damper is a novel semiactive control device whichutilizes piezoelectric stacks to regulate the damping forceto provide a satisfying level of friction force Recently theauthors also proposed a piezoelectric friction damper andinvestigated their performances theoretically and experimen-tally [17]

During the movement of the base-isolated structure afriction damper has two possible motion states sticking andslipping phases [18 19] The friction force of the piezoelectricfriction damper is given as [20]

119873(119905) = 119873pre + 119862pz119881 (119905)

119891 (119905) = minus120583119873 (119905) sgn () = 0

minus120583119873 (119905) le 119891 (119905) le 120583119873 (119905) = 0

(5)

where 119873(119905) is the total contact force 119873pre represents thepreload of the piezoelectric friction damper 119862pz is thepiezoelectric coefficient of the piezoelectric actuator 119881(119905)is the input voltage of piezoelectric stack actuator 120583 is the

Table 3 Parameters of piezoelectric friction damper

Parameters Values120583 04119862pz 1125NV119881max 1000V

friction coefficient of the damper sgn(sdot) represents the signfunction related to the slip rate of the damper and 119891(119905)denotes damping force of piezoelectric friction damper

However the static state of the piezoelectric frictiondamper is complex to be estimated Shook et al [21] proposedan approximate calculation formula for the sticking frictionforce as given in the following

119891119904= minus120583119873 (119905) sgn ()

when 119891119904=1003816100381610038161003816119891119894 + 119891119903

1003816100381610038161003816 1003816100381610038161003816119891 (119905)

1003816100381610038161003816 ge 119891119904

119891119894= 119898119905119892= (119898

119887+

119899

sum

119894=1

119898119894) 119892

119891119903= 119896119887119909119887

(6)

where 119891119894is the inertial force applied on the mass 119891

119903is the

restoring force provided by the isolation bearing 119898119894is the

mass of the superstructure 119898119887and 119896

119887are the mass and

stiffness of base isolator and 119909119887is the displacement of base

isolatorThe parameters of piezoelectric friction damper are listed

in Table 3 And the preload of the piezoelectric frictiondamper can be optimized by genetic algorithm

4 GA-Based Hierarchic Fuzzy ControlAlgorithm

41 Framework of the Developed Fuzzy Logic Controller Thecontroller adopts a hierarchic fuzzy control algorithm inwhich a supervisory fuzzy controller governs a sublevelfuzzy controller by altering its input normalization factorsaccording to the current level of groundmotionThe sublevelfuzzy logic controller is designed to determine the commandvoltage of piezoelectric friction damper according to thevelocity and displacement of base isolation Piezoelectricfriction damper regulates the damping force according tothe input voltage Genetic algorithm is employed to optimizesupervisory fuzzy controller and preload of piezoelectricfriction damper according to an objective function and thegenerated artificial earthquakes for different ground sitesTheblock diagram of the system for the developed controller isshown in Figure 7

42 Sublevel Fuzzy Controller The sublevel fuzzy controlleris established in order to determine the command voltage ofthe piezoelectric friction damper The isolation displacementand velocity are selected as two input variables and commandvoltage is employed as a single output variable as shown inFigure 8The definitions of themembership function of input

Mathematical Problems in Engineering 7

Ground motion

Damping force

Semiactiveisolated

structure

Piezoelectricfriction damper

Ground velocity

Optimize

Voltage

Structural response

Isolation velocity and displacement

Sublevel fuzzycontroller

Supervisoryfuzzy controller

Optimize

Genetic algorithm

Nd

N

Figure 7 Block diagram of the base-isolated system for the fuzzy controller

minus10 minus05 00 05 100

1PL

PMPSZENSNM

Deg

ree o

f mem

bers

hip

Normalized displacement

NL

00 05 100

1PL

PMPSZENSNM

Deg

ree o

f mem

bers

hip

Normalized velocity

NL

0 200 400 600 800 10000

1VL

LMS

Deg

ree o

f mem

bers

hip

Voltage (V)

ZE

minus10 minus05

Figure 8 Input and output membership functions of sublevel fuzzy control

variables are as follows NL negative large NM negativemedium NS negative small ZE zero PS positive small PMpositive medium and PL positive large The definition ofthe membership function of output variable is as follows ZEzero S small M medium L large and VL very large Themembership functions are employed Gaussian type for inputand output variables The fuzzy control rules are defined inTable 4

In the establishment of fuzzy control rules it followsthe following principles if the isolation displacement andvelocity are in opposite sign then the output voltage becomessmall in order to ensure output small damping force inthe piezoelectric friction damper Contrarily if the isolationdisplacement and velocity have the same sign the outputvoltage becomes large Certainly when the displacement andvelocity are almost zero or small the command voltage is

8 Mathematical Problems in Engineering

Table 4 Fuzzy control rules adopted for sublevel fuzzy control

Velocity ofisolated floor

Displacement of isolated floorNL NM NS ZE PS PM PL

NL VL VL L L M S ZENM VL L L M S ZE SNS L L M S ZE S MZE L M S ZE S M LPS M S ZE S M L LPM S ZE S M L L VLPL ZE S M L L VL VL

minus1minus05

005

1

minus1minus05

005

1

500

1000

VelocityDisplacement

Volta

ge (V

)

Figure 9 Fuzzy control surface for sublevel fuzzy controller

about zero this means that piezoelectric friction damper actsas a passive friction damper The defuzzification of fuzzycontrol adopts the method of centroid to get a crisp outputvalue The control surface and color-filled contour line ofsublevel fuzzy control are depicted in Figure 9

43 Supervisory Fuzzy Logic Controller In the fuzzy logiccontrol normalization factors need to satisfy a certain objec-tive The oversize normalization factors can enlarge the basedisplacement effectively Contrarily too small normalizationfactors can result in large control force that amplifies theaccelerations of base-isolated structure Thus a supervisoryfuzzy logic control is proposed to adjust its normalizationfactors in real-time As discussed earlier near-fault earth-quakes usually have long duration pulses with peak velocitiesThus the supervisory fuzzy control employs ground velocityas single input variable to identify the characteristics ofthe ground motion The normalization factors of sublevelfuzzy control are selected as two output variables HereGaussian membership functions are used for input andoutput variables as shown in

120583gauss = exp[minus(119909 minus 119888)2

21205902] (7)

where 119888 and 120590 are the constant values that define the shape ofthe Gauss functions respectively

The rules of the supervisory fuzzy controller are definedby the following form

Rule119894 IF 119883 is 119860119894 then 1198841is 1198621198941 1198842is 1198621198942

119894 = 1 2 119872

(8)

where119872 is the number of fuzzy control rules 119883 is the inputvariable 119884

1and 119884

2are the output variables 119860119894 119862119894

1 and 119862119894

2

are the linguistic values characterized by input and outputmembership functions respectively One fuzzy control ruleis described by three Gaussian membership functions andeach membership function can be defined by two parameters(119888 and 120590) Therefore a total of five fuzzy control rules canbe optimized by encoding these two parameters into thegene using genetic algorithm Consequently a total of 30parameters are encoded into the chromosome to define theinference system of supervisory fuzzy controller as shown inFigure 10

Similar to normalization factors the preload of thepiezoelectric friction dampers has a great influence on thedamping effect Thus it is essential to establish an effectivesupervisory fuzzy logic controller and a suitable preloadof piezoelectric friction damper Generally for the seismicprotection of a base-isolated structure there is a trade-off between the isolation displacement and superstructureacceleration The main control objective is to depress theisolation displacementwithout excessively increasing acceler-ation response of the superstructure In this section a geneticalgorithm is employed to seek out an optimal solution forthe control of the base-isolated structure The flow chart ofgenetic algorithm is shown in Figure 11

Genetic algorithm is a computational model for thesimulation of Darwin natural genetic selection and biologicalevolution Different from the traditional search algorithmgenetic algorithm begins to search a group of optimal solu-tions from an initial random population by mutation andrecombination Each individual which consists of a set ofbinary strings is a solution to the objective problem Afterinitialization genetic algorithm uses a sort method to rankindividuals It compares each solution with other solutionsin the population to find whether it is dominated Duringthe process of creating a new generation it selects a suitableindividual according to the size of the fitness value Afterseveral generations the individual value gradually convergesto the best chromosome which is the optimal solution

The objective fitness function employed in this study isshown as follows

119869 = 06 times119910119887max

119910119887max

+ 04 timesradicsum119899

119894=1(119886119894max119886119894max)

2

119899 (9)

where 119910119887max and 119910119887max denote the peak base displacements

for the fuzzy control and uncontrolled cases respectively119886119894max and 119886119894max represent the peak superstructure accelera-tion for the fuzzy control and uncontrolled case respectively

The objective of genetic algorithm is tomake the objectivefitness function reach its minimum value by selecting oneset of parameters of supervisory fuzzy control and preload

Mathematical Problems in Engineering 9

0

1

X

0

1

Deg

ree o

f mem

bers

hip

Deg

ree o

f mem

bers

hip

0

1

Deg

ree o

f mem

bers

hip

1205901

1205901 1205902 1205903

Rule 1 (1 6) Rule 1 (7 12) Rule 5 (24 30)middot middot middot

c1

c1 c2 c3

1205902

Y1

1205903

Y2c2 c3

Figure 10 Encoding structure for genetic algorithm

of piezoelectric friction damper The initial population sizegenetic algebra and crossover probability are set to 20 50and 08 respectively Through inputting the artificial earth-quakes which are characterized by near-fault earthquakesfor different ground sites the supervisory fuzzy control andpreload of piezoelectric friction dampers can be optimizedThe fuzzy control surfaces of optimized supervisory fuzzycontrol are shown in Figure 12

5 Linear Quadratic Gaussian Controller

LQG (Linear Quadratic Gaussian) method is based onKalman filter technique which has become a widely usedcontrol algorithm For comparison purpose LQG is adoptedto regulate the contact normal force of piezoelectric frictiondamper in the study The optimal controller takes groundacceleration as white noise and considers the velocity anddisplacement of base isolation as feedback signals Thecontrol performance index is defined as follows [22]

119869 = lim120591rarr+infin

1

120591

sdot 119864 int

120591

0

[Z (119905)119879QZ (119905) + U (119905)119879RU (119905)] 119889 (119905) (10)

where Q2119899times2119899

and R1times1

are semi-positive definite matrix andpositive definite matrix respectivelyThe control force can beobtained as follows

U (119905) = minusGZ (119905) (11)

G = Rminus1B119879P (12)

where P can be computed by the solution of the Riccatiequation as follows

minusPA minus A119879P + PBRminus1B119879P minusQ = 0 (13)

The control force obtained from the above equation isactive control force which could not be always achieved bypiezoelectric friction damper It is realized that the directionof active control force is opposite to the slipping direction ofpiezoelectric friction damper Therefore the desired controlforce119906

119889(119905) can be achieved according to the following criteria

119906119889(119905)

=

119891max sgn (119887) (119906active

119887lt 0

10038161003816100381610038161003816119906active10038161003816100381610038161003816 gt 119891max)

10038161003816100381610038161003816119906active10038161003816100381610038161003816 sgn (119887) (119906

active119887lt 0

10038161003816100381610038161003816119906active10038161003816100381610038161003816 le 119891max)

119891min sgn (119887) (119906active

119887ge 0)

(14)

10 Mathematical Problems in Engineering

Table 5 Parameters of base-isolated structure

Floor masses(kg)

Stiffness values(kNm)

Dampingcoefficients(kN sm)

Isolated floor 6800 232 745First floor 5897 33732 67Second floor 5897 29093 58Third floor 5897 28621 57Fourth floor 5897 24954 50Fifth floor 5897 19059 38

No

Yes

Encode

Generate initial random population

Calculate the value of fitness and rank

Copy crossover and mutation

Decode

Optimal solution

Whether or not to meet thecondition of convergence

Figure 11 Flow chart of genetic algorithm

where 119906active is the control force obtained from LQG con-troller

119887is the velocity of base isolator119891max and119891min are the

maximum and minimum friction forces of the piezoelectricfriction damper respectively

6 Numerical Simulations

61 Model of the Base-Isolated Structure A five-story base-isolated building which is proposed by He et al is employedto evaluate the performance of developed fuzzy controllers[18] The fundamental period of the five-story building is03 s For the given isolation parameters the fundamentalperiod of the base-isolated building becomes 25 sThereforean isolation ratio 120575 equal to 83 (=2503) is obtainedThe model of the base-isolated structure with piezoelectricfriction damper is shown in Figure 13 The parameters of thebase-isolated structure are shown in Table 5

62 Performance Evaluation Index In order to evaluate theperformance of base-isolated structure for different controlalgorithms a total of nine performance indexes are employedin this study [23] as shown in Table 6

The performance indexes J1through J

5denote the struc-

ture responses for the controlled building normalized byuncontrolled structure respectively The performance indexJ6evaluates the peak control force normalized by the peak

base shear for controlled structure The performance indexesJ7and J8represent RMS (Root Mean Square) base displace-

ments and RMS floor accelerations respectively J9computes

the energy dissipated by friction dampers normalized by theearthquake input energy to the controlled structure

63 Simulation Results and Analysis A total of nine seis-mic excitations that contain six real ground motions andthree artificial earthquakes are selected to evaluate the per-formance of the optimized fuzzy logic controller In thisstudy the time histories of strong earthquake which rangefrom 20 s to 70 s are selected for numerical simulation andanalysis

The numerical results for various earthquakes are listedin Table 7 In the table the Genetic Algorithm HierarchicFuzzy Logic Control is named as GHFLC Moreover forcomparison purpose the results for an optimal controller andpassive operation of friction damper are also listed in thetable Numbers in bold font indicate the best results amongall control cases

Base displacement is an important index to evaluatethe effectiveness for different controllers For a base-isolatedstructure the reduction of base displacement is a primarypurpose to prevent permanent damage for isolation bearingsor adjacent buildings Although passive operation of frictiondampers can successfully reduce the performance indexassociated with the peak and RMS base displacements (J

3and

J7) it causes significant amplification in peak and RMS floor

accelerations (J5and J

8) for most cases due to the passive

control For example as compared to the uncontrolledstructure for TCU052 TCU053 and TCU054 earthquakespassive control leads to 6 45 and 42 amplification inpeak floor acceleration respectively However the proposedfuzzy controller can successfully improve the base-isolatedstructure acceleration at the cost of slight deterioration in theperformance indices J

3and J7on comparison with passive

control For example for TCU052 TCU053 and TCU054earthquakes GHFLC results in 15 13 and 16 decrease inpeak floor accelerations respectively As compared to passivecontrol there are 9 3 and 7 increase in peak basedisplacements

The time histories of friction force and force-displacement curves of friction dampers for differentcontrollers subjected to TCU052 earthquake are shown inFigure 14 From the figures it can be seen that the passivecontrol outputs lager damper force than GHFLC Becausethe supervisory fuzzy control can alter input normalizationfactors of sublevel FLC according to the current level ofground motion there are some serrations presented at theedge of the hysteretic curve of piezoelectric friction damper

The comparison of the performance indexes J3 J7 J5and

J8under different control cases is shown in Figures 15 and

16 respectively From these figures it can be seen that thefuzzy controller is more effective than passive and optimal

Mathematical Problems in Engineering 11O

utpu

t

009

055

026

000033

000094000

Input ground velocity (ms)

Nd

N

(a) Hard soilO

utpu

t

Input ground velocity (ms)

071

042

000

008000

037

103000

Nd

N

(b) Medium soil

Out

put

Input ground velocity (ms)

107

053

000045

011000

117000

Nd

N

(c) Soft soil

Figure 12 Control surface for optimized supervisory fuzzy control

PFD

Fixed reference

LRB

Figure 13 Model of the base-isolated structure

12 Mathematical Problems in Engineering

Table 6 Performance index

Peak base shear Peak interstory drift RMS base displacement

1198691=max119905

10038171003817100381710038171198810 (119905)1003817100381710038171003817

max119905

100381710038171003817100381710038171198810(119905)10038171003817100381710038171003817

1198694=

max119905119891

10038171003817100381710038171003817119889119891(119905)10038171003817100381710038171003817

max119905119891

10038171003817100381710038171003817119889119891(119905)10038171003817100381710038171003817

1198697=

max119894

1003817100381710038171003817120590119889 (119905)1003817100381710038171003817

max119905

1003817100381710038171003817119889 (119905)1003817100381710038171003817

Peak structural shear Peak floor acceleration RMS floor acceleration

1198692=max119905

10038171003817100381710038171198811 (119905)1003817100381710038171003817

max119905

100381710038171003817100381710038171198811(119905)10038171003817100381710038171003817

1198695=

max119905119891

10038171003817100381710038171003817119886119891(119905)10038171003817100381710038171003817

max119905119891

10038171003817100381710038171003817119886119891(119905)10038171003817100381710038171003817

1198698=max119891

1003817100381710038171003817120590119886 (119905)1003817100381710038171003817

max119891

1003817100381710038171003817119886 (119905)1003817100381710038171003817

Peak base displacement Peak control force Energy dissipated by PFD

1198693=max119905

1003817100381710038171003817119909119887 (119905)1003817100381710038171003817

max119905

1003817100381710038171003817119909119887 (119905)1003817100381710038171003817

1198696=max119905

1003817100381710038171003817119891119889 (119905)1003817100381710038171003817

max119905

10038171003817100381710038171198810 (119905)1003817100381710038171003817

1198699=

int119879

0

119891119889(119905) 119887(119905) 119889119905

int119879

0

1198810(119905) 119892(119905) 119889119905

Table 7 Results of numerical simulation

Earthquake Control case 1198691

1198692

1198693

1198694

1198695

1198696

1198697

1198698

1198699

TCU102(hard site)

Passive 081 082 068 085 094 048 057 082 078Optimal 092 095 075 099 087 043 068 081 069GHFLC 087 091 071 093 082 041 061 078 073

TCU052(hard site)

Passive 079 079 046 082 106 036 038 089 087Optimal 087 087 057 087 098 029 049 085 079GHFLC 083 082 055 082 091 033 044 079 084

Artificialearthquake(hard site)

Passive 072 074 054 076 092 054 049 090 084Optimal 084 086 069 083 089 047 057 086 073GHFLC 076 077 061 079 083 042 052 081 076

TCU053(medium site)

Passive 061 065 039 071 145 032 037 116 089Optimal 069 072 046 076 136 031 045 117 078GHFLC 062 062 042 065 132 026 044 109 072

TCU054(medium site)

Passive 071 073 043 073 142 084 038 121 088Optimal 081 087 045 085 132 079 052 125 086GHFLC 075 071 040 074 126 082 045 113 076

Artificialearthquake(medium site)

Passive 054 057 038 064 123 067 036 117 091Optimal 067 066 047 067 119 078 048 113 079GHFLC 058 061 040 062 113 072 041 109 085

TCU110(soft soil site)

Passive 077 078 047 077 103 050 045 089 095Optimal 083 082 052 085 107 046 052 099 087GHFLC 086 086 056 086 104 042 049 093 090

CHY101(soft soil site)

Passive 069 071 058 075 086 066 054 092 084Optimal 075 073 062 074 087 064 055 088 079GHFLC 063 067 054 067 079 065 051 087 083

Artificialearthquake(soft site)

Passive 057 064 061 068 097 061 058 098 088Optimal 071 070 074 075 094 058 071 093 083GHFLC 065 062 067 069 085 055 063 086 076

controller in simultaneously depressing the superstructureacceleration and base displacement For example the appli-cation of developed fuzzy controller leads to an average of112 decrease in peak floor acceleration and an average ofonly 36 increase in peak base displacement as compared topassive control Particularly optimal controller produces anaverage of only 41 reduction in peak floor acceleration and

leads to 79 increase in peak base displacement as comparedto passive control Therefore the improved fuzzy controlmethod shows better performance than passive and optimalcontrol

In order to further evaluate the performance of differentcontrollers the energy time histories for different controllersare compared with each other For a base-isolated structure

Mathematical Problems in Engineering 13

20 30 40 50 60 70minus20

minus10

00

10

20Fr

ictio

n fo

rce (

kN)

Time (s)minus03 minus02 minus01 00 01 02 03

minus20

minus10

00

10

20

Fric

tion

forc

e (kN

)

Displacement (m)

(a) Passive control

20 30 40 50 60 70minus20

minus10

00

10

20

Fric

tion

forc

e (kN

)

Time (s)minus03 minus02 minus01 00 01 02 03

minus20

minus10

00

10

20

Fric

tion

forc

e (kN

)

Displacement (m)

(b) GHFLC method

Figure 14 Time histories of friction force and force-displacement diagram against TCU052 earthquake

1 2 3 4 5 6 7 8 903

04

05

06

07

08

Excitation case

Passive OptimalGHFLC

1 2 3 4 5 6 7 8 903

04

05

06

07

Excitation casePassive

GHFLC Optimal

J 3 J 5

Figure 15 Comparisons on the performance indexes J3and J7for different control cases

14 Mathematical Problems in Engineering

1 2 3 4 5 6 7 8 907

08

09

10

11

12

13

14

15

Excitation casePassive

GHFLC Optimal

1 2 3 4 5 6 7 8 907

08

09

10

11

12

13

Excitation case

Passive

GHFLC Optimal

J 8J 5

Figure 16 Comparison of the performance indexes J5and J8for different control cases

with piezoelectric friction dampers installed on the isolationthe energy equations are defined as follows

119864119870+ 119864120585+ 119864119878+ 119864119867= 119864119868

119864119870=1

2119879

119905119872119905

119864120585= int

119905

0

119879

119888 119889119905

119864119878= int

119905

0

119909119879

119870119889119909

119864119867= minusint

119905

0

119906119879

119864119879

119904119889119909

119864119868= minusint

119905

0

gMI 119889119909

(15)

where 119864119870 119864120585 119864119878 119864119867 and 119864

119868denote the absolute kinetic

energy damping energy elastic strain energy energy dis-sipated by piezoelectric friction dampers and total inputenergy respectively The energy time histories for differentcontrollers against TCU052Chi-Chi earthquake are shown inFigure 17 It can be seen from the figures that the piezoelectricfriction dampers dissipate most of the input energy fordifferent control cases subjected to TCU052 earthquake

In order to compare different effects under near-faultground motions recorded for different sites the average ofinput energy and structure responses subjected to near-faultearthquakes are given in Table 8

As shown in Table 8 the near-fault earthquakes forsoft sites are more destructive than hard sites For instancecompared to hard sites the input energy and the base dis-placement of RMS of the base-isolated structure for soft soil

increase by 143 and 256 respectively However GHFLCpossesses favorable performance under different ground sitesand the damping effect has no distinctly direct relationshipwith site category

As discussed in Section 61 the isolation ratio of thesimulation model equals 83 In order to evaluate the effectsof isolation ratio on the damping performance of GHFLC thestiffness value of isolation is adjusted to 1045 and 452 kNmrespectively Then the numerical results for different valuesof isolation ratio (120575 = 4 6) are obtained The performanceindexes J

3and J5for different isolation ratios are shown in

Figures 18 and 19 respectivelyFor base-isolated structure isolation ratio has a signifi-

cant influence on the isolation effect A larger isolation ratiowhich means a minor stiffness value of isolation usuallyleads to conspicuous enlargement of base displacement anddecrease of superstructural responses due to the increaseof fundamental vibration period and vice versa Howeveras shown in Figures 18 and 19 the shock absorption rateof GHFLC has little change when isolation ratio variesdifferently and the proposed fuzzy control shows favorableeffectiveness in the diverse isolation ratios of base-isolatedstructures

7 Conclusions

In this study an optimized fuzzy logic control which isdesigned for Chi-Chi near-fault earthquakes under differentground sites is proposed An elastic design spectrum isproposed to generate near-fault earthquakes for differentground sitesThe characteristic of the design spectrum is thatit has larger periods and peak acceleration than conventionalspectrum Genetic algorithm is employed to optimize thesupervisory fuzzy controller and preload of piezoelectric

Mathematical Problems in Engineering 15

Table 8 Average ofinput energy and structure responses subjected to near-fault earthquakes

Site classification Input energy (kNsdotm) Base shear (kN) Base displacement ofRMS (m)

Structure accelerationof RMS (g)

Hard soil 24375 475 0047 0432Medium soil 26746 498 0054 0476Soft soil 27857 568 0059 0531

20 30 40 50 60 7000

05

10

15

20

25

Input energyEnergy dissipated by dampers

Time (s)

Ener

gy (k

Nmiddotm

)

times104

(a) Passive control

20 30 40 50 60 7000

05

10

15

20

25

30

Time (s)

Input energyEnergy dissipated by dampers

Ener

gy (k

Nmiddotm

)

times104

(b) Optimal control

20 30 40 50 60 7000

05

10

15

20

25

30

Input energyEnergy dissipated by dampers

Time (s)

Ener

gy (k

Nmiddotm

)

times104

(c) GHFLC method

Figure 17 Energy time histories subjected to Chi-Chi TCU052 earthquake

friction dampers according to three artificial earthquakesthat are characterized by Chi-Chi earthquakes Passive andoptimal controllers are also compared with the performanceof the developed fuzzy controller The simulation resultsreveal that the developed semiactive fuzzy controller hasbetter performance than traditional passive and optimal con-troller in simultaneously reducing the base displacement and

floor acceleration under near-fault earthquakes for differentground sites

Conflict of Interests

The authors declare no conflict of interests regarding thepublication of this paper

16 Mathematical Problems in Engineering

1 2 3 4 5 6 7 8 903

04

05

06

07

08

Excitation casePassive

GHFLC Optimal

1 2 3 4 5 6 7 8 907

08

09

10

11

12

13

14

15

Excitation case

Passive

GHFLC Optimal

J 3 J 5Figure 18 Comparisons on the performance indexes J

3and J5for different control cases (120575 = 4)

1 2 3 4 5 6 7 8 903

04

05

06

07

08

Excitation casePassive

GHFLC Optimal

1 2 3 4 5 6 7 8 907

08

09

10

11

12

13

14

15

Excitation casePassive

GHFLC Optimal

J 3 J 5

Figure 19 Comparisons on the performance indexes J3and J5for different control cases (120575 = 6)

Acknowledgments

This research was supported by National Natural ScienceFoundation of China under Grant no 51308487 no 41402261and no 51408526 Hebei Provincial Natural Science Founda-tion ofChina underGrant no E2014203055 and the ExcellentYouth Foundation of Hebei Educational Committee underGrant no YQ2013015 The support for this research is greatlyappreciated

References

[1] C Alhan and H Gavin ldquoA parametric study of linear and non-linear passively damped seismic isolation systems for buildingsrdquoEngineering Structures vol 26 no 4 pp 485ndash497 2004

[2] R S Jangid and J M Kelly ldquoBase isolation for near-faultmotionsrdquoEarthquake Engineering and Structural Dynamics vol30 no 5 pp 691ndash707 2001

[3] J Shen M-H Tsai K-C Chang and G C Lee ldquoPerformanceof a seismically isolated bridge under near-fault earthquake

Mathematical Problems in Engineering 17

ground motionsrdquo Journal of Structural Engineering vol 130 no6 pp 861ndash868 2004

[4] F Mazza A Vulcano and M Mazza ldquoNonlinear dynamicresponse of RC buildings with different base Isolation systemssubjected to horizontal and vertical components of near-faultground motionsrdquo Open Construction and Building TechnologyJournal vol 6 pp 373ndash383 2012

[5] F Mazza and A Vulcano ldquoEffects of near-fault ground motionson the nonlinear dynamic response of base-isolated rc framedbuildingsrdquo Earthquake Engineering and Structural Dynamicsvol 41 no 2 pp 211ndash232 2012

[6] O E Ozbulut and S Hurlebaus ldquoFuzzy control of piezoelectricfriction dampers for seismic protection of smart base isolatedbuildingsrdquo Bulletin of Earthquake Engineering vol 8 no 6 pp1435ndash1455 2010

[7] O E Ozbulut M Bitaraf and S Hurlebaus ldquoAdaptive controlof base-isolated structures against near-field earthquakes usingvariable friction dampersrdquo Engineering Structures vol 33 no12 pp 3143ndash3154 2011

[8] J M Kelly ldquoThe role of damping in seismic isolationrdquo Earth-quake Engineering and Structural Dynamics vol 28 no 1 pp3ndash20 1999

[9] F Mazza and A Vulcano ldquoNonlinear response of RC framedbuildings with isolation and supplemental damping at the basesubjected to near-fault earthquakesrdquo Journal of EarthquakeEngineering vol 13 no 5 pp 690ndash715 2009

[10] M Bitaraf and S Hurlebaus ldquoSemi-active adaptive control ofseismically excited 20-story nonlinear buildingrdquo EngineeringStructures vol 56 no 11 pp 2107ndash2118 2013

[11] D Das T K Datta and A Madan ldquoSemiactive fuzzy controlof the seismic response of building frames with MR dampersrdquoEarthquake Engineering and Structural Dynamics vol 41 no 1pp 99ndash118 2012

[12] A-P Wang and C-D Lee ldquoFuzzy sliding mode control for abuilding structure based on genetic algorithmsrdquo EarthquakeEngineering and Structural Dynamics vol 31 no 4 pp 881ndash8952002

[13] D G Reigles and M D Symans ldquoSupervisory fuzzy controlof a base-isolated benchmark building utilizing a neuro-fuzzymodel of controllable fluid viscous dampersrdquo Structural Controland Health Monitoring vol 13 no 2-3 pp 724ndash747 2006

[14] H-S Kim and P N Roschke ldquoGA-fuzzy control of smartbase isolated benchmark building using supervisory controltechniquerdquo Advances in Engineering Software vol 38 no 7 pp453ndash465 2007

[15] D Yang and Y Zhao ldquoEffects of rupture forward directivity andfling step of near-fault groundmotions on seismic performanceof base-isolated building structurerdquo Acta Seismologica Sinicavol 32 no 5 pp 579ndash587 2010

[16] Y E-A Mohamedzein J A Abdalla and A Abdelwahab ldquoSiteresponse and earthquake design spectra for central KhartoumSudanrdquoBulletin of Earthquake Engineering vol 4 no 3 pp 277ndash293 2006

[17] D Zhao and H Li ldquoShaking table tests and analyses of semi-active fuzzy control for structural seismic reduction with apiezoelectric variable-friction damperrdquo Smart Materials andStructures vol 19 no 10 Article ID 105031 2010

[18] W L He A K Agrawal and J N Yang ldquoNovel semiactivefriction controller for linear structures against earthquakesrdquoJournal of Structural Engineering vol 129 no 7 pp 941ndash9502003

[19] J N Yang and A K Agrawal ldquoSemi-active hybrid controlsystems for nonlinear buildings against near-field earthquakesrdquoEngineering Structures vol 24 no 3 pp 271ndash280 2002

[20] O E Ozbulut and S Hurlebaus ldquoOptimal design of supere-lastic-friction base isolators for seismic protection of highwaybridges against near-field earthquakesrdquo Earthquake Engineeringand Structural Dynamics vol 40 no 3 pp 273ndash291 2011

[21] D A Shook P N Roschke and O E Ozbulut ldquoSuperelasticsemi-active damping of a base-isolated structurerdquo StructuralControl and HealthMonitoring vol 15 no 5 pp 746ndash768 2008

[22] K D PhamG JinM K Sain B F Spencer Jr and S R LibertyldquoGeneralized linear quadratic Gaussian techniques for the windbenchmark problemrdquo Journal of Engineering Mechanics vol130 no 4 pp 466ndash470 2004

[23] S Nagarajaiah and S Narasimhan ldquoSmart base-isolated bench-mark building Part II Phase I sample controllers for linearisolation systemsrdquo Structural Control and Health Monitoringvol 13 no 2-3 pp 605ndash625 2006

Submit your manuscripts athttpwwwhindawicom

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

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Mathematical Problems in Engineering

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Differential EquationsInternational Journal of

Volume 2014

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Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Probability and StatisticsHindawi Publishing Corporationhttpwwwhindawicom Volume 2014

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Mathematical PhysicsAdvances in

Complex AnalysisJournal of

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OptimizationJournal of

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CombinatoricsHindawi Publishing Corporationhttpwwwhindawicom Volume 2014

International Journal of

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Operations ResearchAdvances in

Journal of

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Function Spaces

Abstract and Applied AnalysisHindawi Publishing Corporationhttpwwwhindawicom Volume 2014

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Algebra

Discrete Dynamics in Nature and Society

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

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Decision SciencesAdvances in

Discrete MathematicsJournal of

Hindawi Publishing Corporationhttpwwwhindawicom

Volume 2014 Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Stochastic AnalysisInternational Journal of

Mathematical Problems in Engineering 3

Table 1 Selected Chi-Chi near-fault earthquakes

Earthquake Station 119881119904(ms) PGA (g) PGV (cms) PGD (cm) PGVPGA Joyner-Boore

distance (Km) Site classification

Chi-Chi

TCU110 21272 018061 52004 31216 029 1158

Soft soil

CHY101 25889 03829 9128 60731 024 994TCU123 27022 01468 375 3087 026 1491TCU051 35006 019428 42378 57953 022 764TCU060 37542 014895 41859 50693 029 851TCU101 38941 023429 56319 62133 025 211TCU056 4032 015539 38959 47705 026 1048

Medium soil

TCU104 41045 010059 43351 46291 044 1287CHY024 42773 022957 4642 42303 021 962TCU106 45137 015421 38177 30958 025 1497TCU053 45455 018717 43092 61802 023 595TCU054 46069 017207 45145 68386 027 528TCU136 4621 016921 48291 5337 029 827TCU082 47281 019836 51229 69534 026 516TCU063 47614 015751 63518 46961 041 978TCU049 48727 025431 5623 69733 023 376TCU068 48734 046625 25662 36592 056 04TCU116 49309 015476 42122 35828 028 1238TCU103 4941 015845 52488 50567 034 608TCU100 53513 011101 3915 4805 036 1137

Hard soil

TCU109 53513 015941 5711 37649 037 1306TCU087 53869 011697 4241 51865 037 698TCU050 54241 014417 37233 46979 026 949TCU048 55121 013435 42379 51429 032 1353TCU057 55523 011363 39208 51227 035 1183TCU075 57302 030134 79037 70594 027 089TCU052 5791 039658 11656 2212 043 03TCU128 59964 016034 63283 63457 040 1313TCU102 71427 026678 80098 75329 031 149

Table 2Variation of site factors andperiods forChi-Chi earthquakeunder different ground sites

Site 119881119904(ms) 119879

119861(s) 119879

119862(s) 119879

119863(s) 119878 (s) 120572 120573

Hard gt530 028 066 460 109 055 070Medium 390ndash530 040 096 580 113 082 020Soft lt390 060 160 640 116 110 100

As shown in Table 1 the selected seismic records areclassified into three categories which are hard medium andsoft soil site respectively The lower and upper limits foreach parameter of different site are listed in Table 2 Duringthe establishment of the design elastic spectrum the PGAis adjusted to 03 g The elastic design spectrum is obtainedby fitting the average response spectrum curve According tothese considerations the design response spectrum for Chi-Chi earthquake is shown in Figure 2 It can be seen from

the figures that the proposed design spectra are conservativecompared to the average spectrum Owing to the longduration pulses the corner periods are larger than that theEurocode 8 recommends

22 Artificial Earthquakes for Different Ground Sites Basedon the above discussions three artificial earthquakes thatare characterized by Chi-Chi near-fault earthquakes underdifferent ground sites are generated by power spectral densityfunction as shown in Figure 3 The artificial earthquakes arecalculated with a time step of 001 s and the PGA is equalto 03 g Artificial earthquakes for hard medium and softsoil site are shown in Figures 4ndash6 respectively From thesefigures it can be observed that the velocity time histories ofthe generated artificial earthquakes possess obvious pulseswith peak velocities Owing to the similar design spectrumthe time histories of the generated artificial for hard site andmedium site are the same despite several nuances However

4 Mathematical Problems in Engineering

0 2 4 6 8 1000

02

04

06

08

10Sp

ectr

al ac

cele

ratio

n (g

)

Period (s)

Design acceleration spectrumMean spectrum

(a) Hard soil site

0 2 4 6 8 1000

02

04

06

08

10

Spec

tral

acce

lera

tion

(g)

Period (s)

Design acceleration spectrumMean spectrum

(b) Medium soil site

0 2 4 6 8 1000

02

04

06

08

10

Spec

tral

acce

lera

tion

(g)

Period (s)

Design acceleration spectrumMean spectrum

(c) Soft soil site

Figure 2 Design spectrum envelopes for Chi-Chi earthquake

Time

d

I(t)

atb tdtc

b c

I(t) = (ttb)2

I(t) = e03(tc minus t)

Figure 3 Envelop for artificial earthquake

Mathematical Problems in Engineering 5

0 2 4 6 8 10 12 14 16 18 20

minus03

minus02

minus01

00

01

02

03

Acce

lera

tion

(g)

Time (s)

(a) Time history of acceleration

0 2 4 6 8 10 12 14 16 18 20

minus09

minus06

minus03

00

03

06

09

Velo

city

(ms

)

Time (s)

(b) Time history of velocity

Figure 4 Artificial earthquakes for hard soil site

0 2 4 6 8 10 12 14 16 18 20

minus03

minus02

minus01

00

01

02

03

Acce

lera

tion

(g)

Time (s)

(a) Time history of acceleration

0 2 4 6 8 10 12 14 16 18 20

minus09

minus06

minus03

00

03

06

09Ve

loci

ty (m

s)

Time (s)

(b) Time history of velocity

Figure 5 Artificial earthquake for medium soil site

0 2 4 6 8 10 12 14 16 18 20

minus03

minus02

minus01

00

01

02

03

Acce

lera

tion

(g)

Time (s)

(a) Time history of acceleration

0 2 4 6 8 10 12 14 16 18 20

minus09

minus06

minus03

00

03

06

09

Velo

city

(ms

)

Time (s)

(b) Time history of velocity

Figure 6 Artificial earthquake for soft soil site

6 Mathematical Problems in Engineering

the time history of the generated artificial earthquakes for softsoil is distinct with the other Particularly the peak velocityreaches 09ms which is significantly greater than the other

3 Model of Base-Isolated Structure andPiezoelectric Friction Damper

31 Equation of Motion for Base-Isolated Structure Consideran n-degree of freedom base-isolated structure with a piezo-electric friction damper at the isolation floor the dynamicequation of the base-isolated system is given by

MX (119905) + CX (119905) + KX (119905) = B119904U (119905) + E

119904119892(119905) (2)

where M C and K represent 119899 times 119899 mass damping andstiffness matrices respectively X(119905) X(119905) and X(119905) are theacceleration velocity and displacement vectors respectivelyU(119905) is the control force generated by the piezoelectric frictiondamper and

119892(119905) is the earthquake acceleration

Rewriting (2) in state-space form gives

Z (119905) = AZ (119905) + BU (119905) + E119892(119905) (3)

where

Z (119905) = [X (119905)X (119905)

]

E = [0119899times1

Mminus1E119904

]

B = [0119899times1

Mminus1B119904

]

A = [0119899times119899

I119899times119899

minusMminus1K minusMminus1C]

(4)

32 Model of Piezoelectric Friction Damper Piezoelectricfriction damper is a novel semiactive control device whichutilizes piezoelectric stacks to regulate the damping forceto provide a satisfying level of friction force Recently theauthors also proposed a piezoelectric friction damper andinvestigated their performances theoretically and experimen-tally [17]

During the movement of the base-isolated structure afriction damper has two possible motion states sticking andslipping phases [18 19] The friction force of the piezoelectricfriction damper is given as [20]

119873(119905) = 119873pre + 119862pz119881 (119905)

119891 (119905) = minus120583119873 (119905) sgn () = 0

minus120583119873 (119905) le 119891 (119905) le 120583119873 (119905) = 0

(5)

where 119873(119905) is the total contact force 119873pre represents thepreload of the piezoelectric friction damper 119862pz is thepiezoelectric coefficient of the piezoelectric actuator 119881(119905)is the input voltage of piezoelectric stack actuator 120583 is the

Table 3 Parameters of piezoelectric friction damper

Parameters Values120583 04119862pz 1125NV119881max 1000V

friction coefficient of the damper sgn(sdot) represents the signfunction related to the slip rate of the damper and 119891(119905)denotes damping force of piezoelectric friction damper

However the static state of the piezoelectric frictiondamper is complex to be estimated Shook et al [21] proposedan approximate calculation formula for the sticking frictionforce as given in the following

119891119904= minus120583119873 (119905) sgn ()

when 119891119904=1003816100381610038161003816119891119894 + 119891119903

1003816100381610038161003816 1003816100381610038161003816119891 (119905)

1003816100381610038161003816 ge 119891119904

119891119894= 119898119905119892= (119898

119887+

119899

sum

119894=1

119898119894) 119892

119891119903= 119896119887119909119887

(6)

where 119891119894is the inertial force applied on the mass 119891

119903is the

restoring force provided by the isolation bearing 119898119894is the

mass of the superstructure 119898119887and 119896

119887are the mass and

stiffness of base isolator and 119909119887is the displacement of base

isolatorThe parameters of piezoelectric friction damper are listed

in Table 3 And the preload of the piezoelectric frictiondamper can be optimized by genetic algorithm

4 GA-Based Hierarchic Fuzzy ControlAlgorithm

41 Framework of the Developed Fuzzy Logic Controller Thecontroller adopts a hierarchic fuzzy control algorithm inwhich a supervisory fuzzy controller governs a sublevelfuzzy controller by altering its input normalization factorsaccording to the current level of groundmotionThe sublevelfuzzy logic controller is designed to determine the commandvoltage of piezoelectric friction damper according to thevelocity and displacement of base isolation Piezoelectricfriction damper regulates the damping force according tothe input voltage Genetic algorithm is employed to optimizesupervisory fuzzy controller and preload of piezoelectricfriction damper according to an objective function and thegenerated artificial earthquakes for different ground sitesTheblock diagram of the system for the developed controller isshown in Figure 7

42 Sublevel Fuzzy Controller The sublevel fuzzy controlleris established in order to determine the command voltage ofthe piezoelectric friction damper The isolation displacementand velocity are selected as two input variables and commandvoltage is employed as a single output variable as shown inFigure 8The definitions of themembership function of input

Mathematical Problems in Engineering 7

Ground motion

Damping force

Semiactiveisolated

structure

Piezoelectricfriction damper

Ground velocity

Optimize

Voltage

Structural response

Isolation velocity and displacement

Sublevel fuzzycontroller

Supervisoryfuzzy controller

Optimize

Genetic algorithm

Nd

N

Figure 7 Block diagram of the base-isolated system for the fuzzy controller

minus10 minus05 00 05 100

1PL

PMPSZENSNM

Deg

ree o

f mem

bers

hip

Normalized displacement

NL

00 05 100

1PL

PMPSZENSNM

Deg

ree o

f mem

bers

hip

Normalized velocity

NL

0 200 400 600 800 10000

1VL

LMS

Deg

ree o

f mem

bers

hip

Voltage (V)

ZE

minus10 minus05

Figure 8 Input and output membership functions of sublevel fuzzy control

variables are as follows NL negative large NM negativemedium NS negative small ZE zero PS positive small PMpositive medium and PL positive large The definition ofthe membership function of output variable is as follows ZEzero S small M medium L large and VL very large Themembership functions are employed Gaussian type for inputand output variables The fuzzy control rules are defined inTable 4

In the establishment of fuzzy control rules it followsthe following principles if the isolation displacement andvelocity are in opposite sign then the output voltage becomessmall in order to ensure output small damping force inthe piezoelectric friction damper Contrarily if the isolationdisplacement and velocity have the same sign the outputvoltage becomes large Certainly when the displacement andvelocity are almost zero or small the command voltage is

8 Mathematical Problems in Engineering

Table 4 Fuzzy control rules adopted for sublevel fuzzy control

Velocity ofisolated floor

Displacement of isolated floorNL NM NS ZE PS PM PL

NL VL VL L L M S ZENM VL L L M S ZE SNS L L M S ZE S MZE L M S ZE S M LPS M S ZE S M L LPM S ZE S M L L VLPL ZE S M L L VL VL

minus1minus05

005

1

minus1minus05

005

1

500

1000

VelocityDisplacement

Volta

ge (V

)

Figure 9 Fuzzy control surface for sublevel fuzzy controller

about zero this means that piezoelectric friction damper actsas a passive friction damper The defuzzification of fuzzycontrol adopts the method of centroid to get a crisp outputvalue The control surface and color-filled contour line ofsublevel fuzzy control are depicted in Figure 9

43 Supervisory Fuzzy Logic Controller In the fuzzy logiccontrol normalization factors need to satisfy a certain objec-tive The oversize normalization factors can enlarge the basedisplacement effectively Contrarily too small normalizationfactors can result in large control force that amplifies theaccelerations of base-isolated structure Thus a supervisoryfuzzy logic control is proposed to adjust its normalizationfactors in real-time As discussed earlier near-fault earth-quakes usually have long duration pulses with peak velocitiesThus the supervisory fuzzy control employs ground velocityas single input variable to identify the characteristics ofthe ground motion The normalization factors of sublevelfuzzy control are selected as two output variables HereGaussian membership functions are used for input andoutput variables as shown in

120583gauss = exp[minus(119909 minus 119888)2

21205902] (7)

where 119888 and 120590 are the constant values that define the shape ofthe Gauss functions respectively

The rules of the supervisory fuzzy controller are definedby the following form

Rule119894 IF 119883 is 119860119894 then 1198841is 1198621198941 1198842is 1198621198942

119894 = 1 2 119872

(8)

where119872 is the number of fuzzy control rules 119883 is the inputvariable 119884

1and 119884

2are the output variables 119860119894 119862119894

1 and 119862119894

2

are the linguistic values characterized by input and outputmembership functions respectively One fuzzy control ruleis described by three Gaussian membership functions andeach membership function can be defined by two parameters(119888 and 120590) Therefore a total of five fuzzy control rules canbe optimized by encoding these two parameters into thegene using genetic algorithm Consequently a total of 30parameters are encoded into the chromosome to define theinference system of supervisory fuzzy controller as shown inFigure 10

Similar to normalization factors the preload of thepiezoelectric friction dampers has a great influence on thedamping effect Thus it is essential to establish an effectivesupervisory fuzzy logic controller and a suitable preloadof piezoelectric friction damper Generally for the seismicprotection of a base-isolated structure there is a trade-off between the isolation displacement and superstructureacceleration The main control objective is to depress theisolation displacementwithout excessively increasing acceler-ation response of the superstructure In this section a geneticalgorithm is employed to seek out an optimal solution forthe control of the base-isolated structure The flow chart ofgenetic algorithm is shown in Figure 11

Genetic algorithm is a computational model for thesimulation of Darwin natural genetic selection and biologicalevolution Different from the traditional search algorithmgenetic algorithm begins to search a group of optimal solu-tions from an initial random population by mutation andrecombination Each individual which consists of a set ofbinary strings is a solution to the objective problem Afterinitialization genetic algorithm uses a sort method to rankindividuals It compares each solution with other solutionsin the population to find whether it is dominated Duringthe process of creating a new generation it selects a suitableindividual according to the size of the fitness value Afterseveral generations the individual value gradually convergesto the best chromosome which is the optimal solution

The objective fitness function employed in this study isshown as follows

119869 = 06 times119910119887max

119910119887max

+ 04 timesradicsum119899

119894=1(119886119894max119886119894max)

2

119899 (9)

where 119910119887max and 119910119887max denote the peak base displacements

for the fuzzy control and uncontrolled cases respectively119886119894max and 119886119894max represent the peak superstructure accelera-tion for the fuzzy control and uncontrolled case respectively

The objective of genetic algorithm is tomake the objectivefitness function reach its minimum value by selecting oneset of parameters of supervisory fuzzy control and preload

Mathematical Problems in Engineering 9

0

1

X

0

1

Deg

ree o

f mem

bers

hip

Deg

ree o

f mem

bers

hip

0

1

Deg

ree o

f mem

bers

hip

1205901

1205901 1205902 1205903

Rule 1 (1 6) Rule 1 (7 12) Rule 5 (24 30)middot middot middot

c1

c1 c2 c3

1205902

Y1

1205903

Y2c2 c3

Figure 10 Encoding structure for genetic algorithm

of piezoelectric friction damper The initial population sizegenetic algebra and crossover probability are set to 20 50and 08 respectively Through inputting the artificial earth-quakes which are characterized by near-fault earthquakesfor different ground sites the supervisory fuzzy control andpreload of piezoelectric friction dampers can be optimizedThe fuzzy control surfaces of optimized supervisory fuzzycontrol are shown in Figure 12

5 Linear Quadratic Gaussian Controller

LQG (Linear Quadratic Gaussian) method is based onKalman filter technique which has become a widely usedcontrol algorithm For comparison purpose LQG is adoptedto regulate the contact normal force of piezoelectric frictiondamper in the study The optimal controller takes groundacceleration as white noise and considers the velocity anddisplacement of base isolation as feedback signals Thecontrol performance index is defined as follows [22]

119869 = lim120591rarr+infin

1

120591

sdot 119864 int

120591

0

[Z (119905)119879QZ (119905) + U (119905)119879RU (119905)] 119889 (119905) (10)

where Q2119899times2119899

and R1times1

are semi-positive definite matrix andpositive definite matrix respectivelyThe control force can beobtained as follows

U (119905) = minusGZ (119905) (11)

G = Rminus1B119879P (12)

where P can be computed by the solution of the Riccatiequation as follows

minusPA minus A119879P + PBRminus1B119879P minusQ = 0 (13)

The control force obtained from the above equation isactive control force which could not be always achieved bypiezoelectric friction damper It is realized that the directionof active control force is opposite to the slipping direction ofpiezoelectric friction damper Therefore the desired controlforce119906

119889(119905) can be achieved according to the following criteria

119906119889(119905)

=

119891max sgn (119887) (119906active

119887lt 0

10038161003816100381610038161003816119906active10038161003816100381610038161003816 gt 119891max)

10038161003816100381610038161003816119906active10038161003816100381610038161003816 sgn (119887) (119906

active119887lt 0

10038161003816100381610038161003816119906active10038161003816100381610038161003816 le 119891max)

119891min sgn (119887) (119906active

119887ge 0)

(14)

10 Mathematical Problems in Engineering

Table 5 Parameters of base-isolated structure

Floor masses(kg)

Stiffness values(kNm)

Dampingcoefficients(kN sm)

Isolated floor 6800 232 745First floor 5897 33732 67Second floor 5897 29093 58Third floor 5897 28621 57Fourth floor 5897 24954 50Fifth floor 5897 19059 38

No

Yes

Encode

Generate initial random population

Calculate the value of fitness and rank

Copy crossover and mutation

Decode

Optimal solution

Whether or not to meet thecondition of convergence

Figure 11 Flow chart of genetic algorithm

where 119906active is the control force obtained from LQG con-troller

119887is the velocity of base isolator119891max and119891min are the

maximum and minimum friction forces of the piezoelectricfriction damper respectively

6 Numerical Simulations

61 Model of the Base-Isolated Structure A five-story base-isolated building which is proposed by He et al is employedto evaluate the performance of developed fuzzy controllers[18] The fundamental period of the five-story building is03 s For the given isolation parameters the fundamentalperiod of the base-isolated building becomes 25 sThereforean isolation ratio 120575 equal to 83 (=2503) is obtainedThe model of the base-isolated structure with piezoelectricfriction damper is shown in Figure 13 The parameters of thebase-isolated structure are shown in Table 5

62 Performance Evaluation Index In order to evaluate theperformance of base-isolated structure for different controlalgorithms a total of nine performance indexes are employedin this study [23] as shown in Table 6

The performance indexes J1through J

5denote the struc-

ture responses for the controlled building normalized byuncontrolled structure respectively The performance indexJ6evaluates the peak control force normalized by the peak

base shear for controlled structure The performance indexesJ7and J8represent RMS (Root Mean Square) base displace-

ments and RMS floor accelerations respectively J9computes

the energy dissipated by friction dampers normalized by theearthquake input energy to the controlled structure

63 Simulation Results and Analysis A total of nine seis-mic excitations that contain six real ground motions andthree artificial earthquakes are selected to evaluate the per-formance of the optimized fuzzy logic controller In thisstudy the time histories of strong earthquake which rangefrom 20 s to 70 s are selected for numerical simulation andanalysis

The numerical results for various earthquakes are listedin Table 7 In the table the Genetic Algorithm HierarchicFuzzy Logic Control is named as GHFLC Moreover forcomparison purpose the results for an optimal controller andpassive operation of friction damper are also listed in thetable Numbers in bold font indicate the best results amongall control cases

Base displacement is an important index to evaluatethe effectiveness for different controllers For a base-isolatedstructure the reduction of base displacement is a primarypurpose to prevent permanent damage for isolation bearingsor adjacent buildings Although passive operation of frictiondampers can successfully reduce the performance indexassociated with the peak and RMS base displacements (J

3and

J7) it causes significant amplification in peak and RMS floor

accelerations (J5and J

8) for most cases due to the passive

control For example as compared to the uncontrolledstructure for TCU052 TCU053 and TCU054 earthquakespassive control leads to 6 45 and 42 amplification inpeak floor acceleration respectively However the proposedfuzzy controller can successfully improve the base-isolatedstructure acceleration at the cost of slight deterioration in theperformance indices J

3and J7on comparison with passive

control For example for TCU052 TCU053 and TCU054earthquakes GHFLC results in 15 13 and 16 decrease inpeak floor accelerations respectively As compared to passivecontrol there are 9 3 and 7 increase in peak basedisplacements

The time histories of friction force and force-displacement curves of friction dampers for differentcontrollers subjected to TCU052 earthquake are shown inFigure 14 From the figures it can be seen that the passivecontrol outputs lager damper force than GHFLC Becausethe supervisory fuzzy control can alter input normalizationfactors of sublevel FLC according to the current level ofground motion there are some serrations presented at theedge of the hysteretic curve of piezoelectric friction damper

The comparison of the performance indexes J3 J7 J5and

J8under different control cases is shown in Figures 15 and

16 respectively From these figures it can be seen that thefuzzy controller is more effective than passive and optimal

Mathematical Problems in Engineering 11O

utpu

t

009

055

026

000033

000094000

Input ground velocity (ms)

Nd

N

(a) Hard soilO

utpu

t

Input ground velocity (ms)

071

042

000

008000

037

103000

Nd

N

(b) Medium soil

Out

put

Input ground velocity (ms)

107

053

000045

011000

117000

Nd

N

(c) Soft soil

Figure 12 Control surface for optimized supervisory fuzzy control

PFD

Fixed reference

LRB

Figure 13 Model of the base-isolated structure

12 Mathematical Problems in Engineering

Table 6 Performance index

Peak base shear Peak interstory drift RMS base displacement

1198691=max119905

10038171003817100381710038171198810 (119905)1003817100381710038171003817

max119905

100381710038171003817100381710038171198810(119905)10038171003817100381710038171003817

1198694=

max119905119891

10038171003817100381710038171003817119889119891(119905)10038171003817100381710038171003817

max119905119891

10038171003817100381710038171003817119889119891(119905)10038171003817100381710038171003817

1198697=

max119894

1003817100381710038171003817120590119889 (119905)1003817100381710038171003817

max119905

1003817100381710038171003817119889 (119905)1003817100381710038171003817

Peak structural shear Peak floor acceleration RMS floor acceleration

1198692=max119905

10038171003817100381710038171198811 (119905)1003817100381710038171003817

max119905

100381710038171003817100381710038171198811(119905)10038171003817100381710038171003817

1198695=

max119905119891

10038171003817100381710038171003817119886119891(119905)10038171003817100381710038171003817

max119905119891

10038171003817100381710038171003817119886119891(119905)10038171003817100381710038171003817

1198698=max119891

1003817100381710038171003817120590119886 (119905)1003817100381710038171003817

max119891

1003817100381710038171003817119886 (119905)1003817100381710038171003817

Peak base displacement Peak control force Energy dissipated by PFD

1198693=max119905

1003817100381710038171003817119909119887 (119905)1003817100381710038171003817

max119905

1003817100381710038171003817119909119887 (119905)1003817100381710038171003817

1198696=max119905

1003817100381710038171003817119891119889 (119905)1003817100381710038171003817

max119905

10038171003817100381710038171198810 (119905)1003817100381710038171003817

1198699=

int119879

0

119891119889(119905) 119887(119905) 119889119905

int119879

0

1198810(119905) 119892(119905) 119889119905

Table 7 Results of numerical simulation

Earthquake Control case 1198691

1198692

1198693

1198694

1198695

1198696

1198697

1198698

1198699

TCU102(hard site)

Passive 081 082 068 085 094 048 057 082 078Optimal 092 095 075 099 087 043 068 081 069GHFLC 087 091 071 093 082 041 061 078 073

TCU052(hard site)

Passive 079 079 046 082 106 036 038 089 087Optimal 087 087 057 087 098 029 049 085 079GHFLC 083 082 055 082 091 033 044 079 084

Artificialearthquake(hard site)

Passive 072 074 054 076 092 054 049 090 084Optimal 084 086 069 083 089 047 057 086 073GHFLC 076 077 061 079 083 042 052 081 076

TCU053(medium site)

Passive 061 065 039 071 145 032 037 116 089Optimal 069 072 046 076 136 031 045 117 078GHFLC 062 062 042 065 132 026 044 109 072

TCU054(medium site)

Passive 071 073 043 073 142 084 038 121 088Optimal 081 087 045 085 132 079 052 125 086GHFLC 075 071 040 074 126 082 045 113 076

Artificialearthquake(medium site)

Passive 054 057 038 064 123 067 036 117 091Optimal 067 066 047 067 119 078 048 113 079GHFLC 058 061 040 062 113 072 041 109 085

TCU110(soft soil site)

Passive 077 078 047 077 103 050 045 089 095Optimal 083 082 052 085 107 046 052 099 087GHFLC 086 086 056 086 104 042 049 093 090

CHY101(soft soil site)

Passive 069 071 058 075 086 066 054 092 084Optimal 075 073 062 074 087 064 055 088 079GHFLC 063 067 054 067 079 065 051 087 083

Artificialearthquake(soft site)

Passive 057 064 061 068 097 061 058 098 088Optimal 071 070 074 075 094 058 071 093 083GHFLC 065 062 067 069 085 055 063 086 076

controller in simultaneously depressing the superstructureacceleration and base displacement For example the appli-cation of developed fuzzy controller leads to an average of112 decrease in peak floor acceleration and an average ofonly 36 increase in peak base displacement as compared topassive control Particularly optimal controller produces anaverage of only 41 reduction in peak floor acceleration and

leads to 79 increase in peak base displacement as comparedto passive control Therefore the improved fuzzy controlmethod shows better performance than passive and optimalcontrol

In order to further evaluate the performance of differentcontrollers the energy time histories for different controllersare compared with each other For a base-isolated structure

Mathematical Problems in Engineering 13

20 30 40 50 60 70minus20

minus10

00

10

20Fr

ictio

n fo

rce (

kN)

Time (s)minus03 minus02 minus01 00 01 02 03

minus20

minus10

00

10

20

Fric

tion

forc

e (kN

)

Displacement (m)

(a) Passive control

20 30 40 50 60 70minus20

minus10

00

10

20

Fric

tion

forc

e (kN

)

Time (s)minus03 minus02 minus01 00 01 02 03

minus20

minus10

00

10

20

Fric

tion

forc

e (kN

)

Displacement (m)

(b) GHFLC method

Figure 14 Time histories of friction force and force-displacement diagram against TCU052 earthquake

1 2 3 4 5 6 7 8 903

04

05

06

07

08

Excitation case

Passive OptimalGHFLC

1 2 3 4 5 6 7 8 903

04

05

06

07

Excitation casePassive

GHFLC Optimal

J 3 J 5

Figure 15 Comparisons on the performance indexes J3and J7for different control cases

14 Mathematical Problems in Engineering

1 2 3 4 5 6 7 8 907

08

09

10

11

12

13

14

15

Excitation casePassive

GHFLC Optimal

1 2 3 4 5 6 7 8 907

08

09

10

11

12

13

Excitation case

Passive

GHFLC Optimal

J 8J 5

Figure 16 Comparison of the performance indexes J5and J8for different control cases

with piezoelectric friction dampers installed on the isolationthe energy equations are defined as follows

119864119870+ 119864120585+ 119864119878+ 119864119867= 119864119868

119864119870=1

2119879

119905119872119905

119864120585= int

119905

0

119879

119888 119889119905

119864119878= int

119905

0

119909119879

119870119889119909

119864119867= minusint

119905

0

119906119879

119864119879

119904119889119909

119864119868= minusint

119905

0

gMI 119889119909

(15)

where 119864119870 119864120585 119864119878 119864119867 and 119864

119868denote the absolute kinetic

energy damping energy elastic strain energy energy dis-sipated by piezoelectric friction dampers and total inputenergy respectively The energy time histories for differentcontrollers against TCU052Chi-Chi earthquake are shown inFigure 17 It can be seen from the figures that the piezoelectricfriction dampers dissipate most of the input energy fordifferent control cases subjected to TCU052 earthquake

In order to compare different effects under near-faultground motions recorded for different sites the average ofinput energy and structure responses subjected to near-faultearthquakes are given in Table 8

As shown in Table 8 the near-fault earthquakes forsoft sites are more destructive than hard sites For instancecompared to hard sites the input energy and the base dis-placement of RMS of the base-isolated structure for soft soil

increase by 143 and 256 respectively However GHFLCpossesses favorable performance under different ground sitesand the damping effect has no distinctly direct relationshipwith site category

As discussed in Section 61 the isolation ratio of thesimulation model equals 83 In order to evaluate the effectsof isolation ratio on the damping performance of GHFLC thestiffness value of isolation is adjusted to 1045 and 452 kNmrespectively Then the numerical results for different valuesof isolation ratio (120575 = 4 6) are obtained The performanceindexes J

3and J5for different isolation ratios are shown in

Figures 18 and 19 respectivelyFor base-isolated structure isolation ratio has a signifi-

cant influence on the isolation effect A larger isolation ratiowhich means a minor stiffness value of isolation usuallyleads to conspicuous enlargement of base displacement anddecrease of superstructural responses due to the increaseof fundamental vibration period and vice versa Howeveras shown in Figures 18 and 19 the shock absorption rateof GHFLC has little change when isolation ratio variesdifferently and the proposed fuzzy control shows favorableeffectiveness in the diverse isolation ratios of base-isolatedstructures

7 Conclusions

In this study an optimized fuzzy logic control which isdesigned for Chi-Chi near-fault earthquakes under differentground sites is proposed An elastic design spectrum isproposed to generate near-fault earthquakes for differentground sitesThe characteristic of the design spectrum is thatit has larger periods and peak acceleration than conventionalspectrum Genetic algorithm is employed to optimize thesupervisory fuzzy controller and preload of piezoelectric

Mathematical Problems in Engineering 15

Table 8 Average ofinput energy and structure responses subjected to near-fault earthquakes

Site classification Input energy (kNsdotm) Base shear (kN) Base displacement ofRMS (m)

Structure accelerationof RMS (g)

Hard soil 24375 475 0047 0432Medium soil 26746 498 0054 0476Soft soil 27857 568 0059 0531

20 30 40 50 60 7000

05

10

15

20

25

Input energyEnergy dissipated by dampers

Time (s)

Ener

gy (k

Nmiddotm

)

times104

(a) Passive control

20 30 40 50 60 7000

05

10

15

20

25

30

Time (s)

Input energyEnergy dissipated by dampers

Ener

gy (k

Nmiddotm

)

times104

(b) Optimal control

20 30 40 50 60 7000

05

10

15

20

25

30

Input energyEnergy dissipated by dampers

Time (s)

Ener

gy (k

Nmiddotm

)

times104

(c) GHFLC method

Figure 17 Energy time histories subjected to Chi-Chi TCU052 earthquake

friction dampers according to three artificial earthquakesthat are characterized by Chi-Chi earthquakes Passive andoptimal controllers are also compared with the performanceof the developed fuzzy controller The simulation resultsreveal that the developed semiactive fuzzy controller hasbetter performance than traditional passive and optimal con-troller in simultaneously reducing the base displacement and

floor acceleration under near-fault earthquakes for differentground sites

Conflict of Interests

The authors declare no conflict of interests regarding thepublication of this paper

16 Mathematical Problems in Engineering

1 2 3 4 5 6 7 8 903

04

05

06

07

08

Excitation casePassive

GHFLC Optimal

1 2 3 4 5 6 7 8 907

08

09

10

11

12

13

14

15

Excitation case

Passive

GHFLC Optimal

J 3 J 5Figure 18 Comparisons on the performance indexes J

3and J5for different control cases (120575 = 4)

1 2 3 4 5 6 7 8 903

04

05

06

07

08

Excitation casePassive

GHFLC Optimal

1 2 3 4 5 6 7 8 907

08

09

10

11

12

13

14

15

Excitation casePassive

GHFLC Optimal

J 3 J 5

Figure 19 Comparisons on the performance indexes J3and J5for different control cases (120575 = 6)

Acknowledgments

This research was supported by National Natural ScienceFoundation of China under Grant no 51308487 no 41402261and no 51408526 Hebei Provincial Natural Science Founda-tion ofChina underGrant no E2014203055 and the ExcellentYouth Foundation of Hebei Educational Committee underGrant no YQ2013015 The support for this research is greatlyappreciated

References

[1] C Alhan and H Gavin ldquoA parametric study of linear and non-linear passively damped seismic isolation systems for buildingsrdquoEngineering Structures vol 26 no 4 pp 485ndash497 2004

[2] R S Jangid and J M Kelly ldquoBase isolation for near-faultmotionsrdquoEarthquake Engineering and Structural Dynamics vol30 no 5 pp 691ndash707 2001

[3] J Shen M-H Tsai K-C Chang and G C Lee ldquoPerformanceof a seismically isolated bridge under near-fault earthquake

Mathematical Problems in Engineering 17

ground motionsrdquo Journal of Structural Engineering vol 130 no6 pp 861ndash868 2004

[4] F Mazza A Vulcano and M Mazza ldquoNonlinear dynamicresponse of RC buildings with different base Isolation systemssubjected to horizontal and vertical components of near-faultground motionsrdquo Open Construction and Building TechnologyJournal vol 6 pp 373ndash383 2012

[5] F Mazza and A Vulcano ldquoEffects of near-fault ground motionson the nonlinear dynamic response of base-isolated rc framedbuildingsrdquo Earthquake Engineering and Structural Dynamicsvol 41 no 2 pp 211ndash232 2012

[6] O E Ozbulut and S Hurlebaus ldquoFuzzy control of piezoelectricfriction dampers for seismic protection of smart base isolatedbuildingsrdquo Bulletin of Earthquake Engineering vol 8 no 6 pp1435ndash1455 2010

[7] O E Ozbulut M Bitaraf and S Hurlebaus ldquoAdaptive controlof base-isolated structures against near-field earthquakes usingvariable friction dampersrdquo Engineering Structures vol 33 no12 pp 3143ndash3154 2011

[8] J M Kelly ldquoThe role of damping in seismic isolationrdquo Earth-quake Engineering and Structural Dynamics vol 28 no 1 pp3ndash20 1999

[9] F Mazza and A Vulcano ldquoNonlinear response of RC framedbuildings with isolation and supplemental damping at the basesubjected to near-fault earthquakesrdquo Journal of EarthquakeEngineering vol 13 no 5 pp 690ndash715 2009

[10] M Bitaraf and S Hurlebaus ldquoSemi-active adaptive control ofseismically excited 20-story nonlinear buildingrdquo EngineeringStructures vol 56 no 11 pp 2107ndash2118 2013

[11] D Das T K Datta and A Madan ldquoSemiactive fuzzy controlof the seismic response of building frames with MR dampersrdquoEarthquake Engineering and Structural Dynamics vol 41 no 1pp 99ndash118 2012

[12] A-P Wang and C-D Lee ldquoFuzzy sliding mode control for abuilding structure based on genetic algorithmsrdquo EarthquakeEngineering and Structural Dynamics vol 31 no 4 pp 881ndash8952002

[13] D G Reigles and M D Symans ldquoSupervisory fuzzy controlof a base-isolated benchmark building utilizing a neuro-fuzzymodel of controllable fluid viscous dampersrdquo Structural Controland Health Monitoring vol 13 no 2-3 pp 724ndash747 2006

[14] H-S Kim and P N Roschke ldquoGA-fuzzy control of smartbase isolated benchmark building using supervisory controltechniquerdquo Advances in Engineering Software vol 38 no 7 pp453ndash465 2007

[15] D Yang and Y Zhao ldquoEffects of rupture forward directivity andfling step of near-fault groundmotions on seismic performanceof base-isolated building structurerdquo Acta Seismologica Sinicavol 32 no 5 pp 579ndash587 2010

[16] Y E-A Mohamedzein J A Abdalla and A Abdelwahab ldquoSiteresponse and earthquake design spectra for central KhartoumSudanrdquoBulletin of Earthquake Engineering vol 4 no 3 pp 277ndash293 2006

[17] D Zhao and H Li ldquoShaking table tests and analyses of semi-active fuzzy control for structural seismic reduction with apiezoelectric variable-friction damperrdquo Smart Materials andStructures vol 19 no 10 Article ID 105031 2010

[18] W L He A K Agrawal and J N Yang ldquoNovel semiactivefriction controller for linear structures against earthquakesrdquoJournal of Structural Engineering vol 129 no 7 pp 941ndash9502003

[19] J N Yang and A K Agrawal ldquoSemi-active hybrid controlsystems for nonlinear buildings against near-field earthquakesrdquoEngineering Structures vol 24 no 3 pp 271ndash280 2002

[20] O E Ozbulut and S Hurlebaus ldquoOptimal design of supere-lastic-friction base isolators for seismic protection of highwaybridges against near-field earthquakesrdquo Earthquake Engineeringand Structural Dynamics vol 40 no 3 pp 273ndash291 2011

[21] D A Shook P N Roschke and O E Ozbulut ldquoSuperelasticsemi-active damping of a base-isolated structurerdquo StructuralControl and HealthMonitoring vol 15 no 5 pp 746ndash768 2008

[22] K D PhamG JinM K Sain B F Spencer Jr and S R LibertyldquoGeneralized linear quadratic Gaussian techniques for the windbenchmark problemrdquo Journal of Engineering Mechanics vol130 no 4 pp 466ndash470 2004

[23] S Nagarajaiah and S Narasimhan ldquoSmart base-isolated bench-mark building Part II Phase I sample controllers for linearisolation systemsrdquo Structural Control and Health Monitoringvol 13 no 2-3 pp 605ndash625 2006

Submit your manuscripts athttpwwwhindawicom

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

MathematicsJournal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Mathematical Problems in Engineering

Hindawi Publishing Corporationhttpwwwhindawicom

Differential EquationsInternational Journal of

Volume 2014

Applied MathematicsJournal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Probability and StatisticsHindawi Publishing Corporationhttpwwwhindawicom Volume 2014

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Mathematical PhysicsAdvances in

Complex AnalysisJournal of

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OptimizationJournal of

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CombinatoricsHindawi Publishing Corporationhttpwwwhindawicom Volume 2014

International Journal of

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Journal of

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Function Spaces

Abstract and Applied AnalysisHindawi Publishing Corporationhttpwwwhindawicom Volume 2014

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Algebra

Discrete Dynamics in Nature and Society

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

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Decision SciencesAdvances in

Discrete MathematicsJournal of

Hindawi Publishing Corporationhttpwwwhindawicom

Volume 2014 Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Stochastic AnalysisInternational Journal of

4 Mathematical Problems in Engineering

0 2 4 6 8 1000

02

04

06

08

10Sp

ectr

al ac

cele

ratio

n (g

)

Period (s)

Design acceleration spectrumMean spectrum

(a) Hard soil site

0 2 4 6 8 1000

02

04

06

08

10

Spec

tral

acce

lera

tion

(g)

Period (s)

Design acceleration spectrumMean spectrum

(b) Medium soil site

0 2 4 6 8 1000

02

04

06

08

10

Spec

tral

acce

lera

tion

(g)

Period (s)

Design acceleration spectrumMean spectrum

(c) Soft soil site

Figure 2 Design spectrum envelopes for Chi-Chi earthquake

Time

d

I(t)

atb tdtc

b c

I(t) = (ttb)2

I(t) = e03(tc minus t)

Figure 3 Envelop for artificial earthquake

Mathematical Problems in Engineering 5

0 2 4 6 8 10 12 14 16 18 20

minus03

minus02

minus01

00

01

02

03

Acce

lera

tion

(g)

Time (s)

(a) Time history of acceleration

0 2 4 6 8 10 12 14 16 18 20

minus09

minus06

minus03

00

03

06

09

Velo

city

(ms

)

Time (s)

(b) Time history of velocity

Figure 4 Artificial earthquakes for hard soil site

0 2 4 6 8 10 12 14 16 18 20

minus03

minus02

minus01

00

01

02

03

Acce

lera

tion

(g)

Time (s)

(a) Time history of acceleration

0 2 4 6 8 10 12 14 16 18 20

minus09

minus06

minus03

00

03

06

09Ve

loci

ty (m

s)

Time (s)

(b) Time history of velocity

Figure 5 Artificial earthquake for medium soil site

0 2 4 6 8 10 12 14 16 18 20

minus03

minus02

minus01

00

01

02

03

Acce

lera

tion

(g)

Time (s)

(a) Time history of acceleration

0 2 4 6 8 10 12 14 16 18 20

minus09

minus06

minus03

00

03

06

09

Velo

city

(ms

)

Time (s)

(b) Time history of velocity

Figure 6 Artificial earthquake for soft soil site

6 Mathematical Problems in Engineering

the time history of the generated artificial earthquakes for softsoil is distinct with the other Particularly the peak velocityreaches 09ms which is significantly greater than the other

3 Model of Base-Isolated Structure andPiezoelectric Friction Damper

31 Equation of Motion for Base-Isolated Structure Consideran n-degree of freedom base-isolated structure with a piezo-electric friction damper at the isolation floor the dynamicequation of the base-isolated system is given by

MX (119905) + CX (119905) + KX (119905) = B119904U (119905) + E

119904119892(119905) (2)

where M C and K represent 119899 times 119899 mass damping andstiffness matrices respectively X(119905) X(119905) and X(119905) are theacceleration velocity and displacement vectors respectivelyU(119905) is the control force generated by the piezoelectric frictiondamper and

119892(119905) is the earthquake acceleration

Rewriting (2) in state-space form gives

Z (119905) = AZ (119905) + BU (119905) + E119892(119905) (3)

where

Z (119905) = [X (119905)X (119905)

]

E = [0119899times1

Mminus1E119904

]

B = [0119899times1

Mminus1B119904

]

A = [0119899times119899

I119899times119899

minusMminus1K minusMminus1C]

(4)

32 Model of Piezoelectric Friction Damper Piezoelectricfriction damper is a novel semiactive control device whichutilizes piezoelectric stacks to regulate the damping forceto provide a satisfying level of friction force Recently theauthors also proposed a piezoelectric friction damper andinvestigated their performances theoretically and experimen-tally [17]

During the movement of the base-isolated structure afriction damper has two possible motion states sticking andslipping phases [18 19] The friction force of the piezoelectricfriction damper is given as [20]

119873(119905) = 119873pre + 119862pz119881 (119905)

119891 (119905) = minus120583119873 (119905) sgn () = 0

minus120583119873 (119905) le 119891 (119905) le 120583119873 (119905) = 0

(5)

where 119873(119905) is the total contact force 119873pre represents thepreload of the piezoelectric friction damper 119862pz is thepiezoelectric coefficient of the piezoelectric actuator 119881(119905)is the input voltage of piezoelectric stack actuator 120583 is the

Table 3 Parameters of piezoelectric friction damper

Parameters Values120583 04119862pz 1125NV119881max 1000V

friction coefficient of the damper sgn(sdot) represents the signfunction related to the slip rate of the damper and 119891(119905)denotes damping force of piezoelectric friction damper

However the static state of the piezoelectric frictiondamper is complex to be estimated Shook et al [21] proposedan approximate calculation formula for the sticking frictionforce as given in the following

119891119904= minus120583119873 (119905) sgn ()

when 119891119904=1003816100381610038161003816119891119894 + 119891119903

1003816100381610038161003816 1003816100381610038161003816119891 (119905)

1003816100381610038161003816 ge 119891119904

119891119894= 119898119905119892= (119898

119887+

119899

sum

119894=1

119898119894) 119892

119891119903= 119896119887119909119887

(6)

where 119891119894is the inertial force applied on the mass 119891

119903is the

restoring force provided by the isolation bearing 119898119894is the

mass of the superstructure 119898119887and 119896

119887are the mass and

stiffness of base isolator and 119909119887is the displacement of base

isolatorThe parameters of piezoelectric friction damper are listed

in Table 3 And the preload of the piezoelectric frictiondamper can be optimized by genetic algorithm

4 GA-Based Hierarchic Fuzzy ControlAlgorithm

41 Framework of the Developed Fuzzy Logic Controller Thecontroller adopts a hierarchic fuzzy control algorithm inwhich a supervisory fuzzy controller governs a sublevelfuzzy controller by altering its input normalization factorsaccording to the current level of groundmotionThe sublevelfuzzy logic controller is designed to determine the commandvoltage of piezoelectric friction damper according to thevelocity and displacement of base isolation Piezoelectricfriction damper regulates the damping force according tothe input voltage Genetic algorithm is employed to optimizesupervisory fuzzy controller and preload of piezoelectricfriction damper according to an objective function and thegenerated artificial earthquakes for different ground sitesTheblock diagram of the system for the developed controller isshown in Figure 7

42 Sublevel Fuzzy Controller The sublevel fuzzy controlleris established in order to determine the command voltage ofthe piezoelectric friction damper The isolation displacementand velocity are selected as two input variables and commandvoltage is employed as a single output variable as shown inFigure 8The definitions of themembership function of input

Mathematical Problems in Engineering 7

Ground motion

Damping force

Semiactiveisolated

structure

Piezoelectricfriction damper

Ground velocity

Optimize

Voltage

Structural response

Isolation velocity and displacement

Sublevel fuzzycontroller

Supervisoryfuzzy controller

Optimize

Genetic algorithm

Nd

N

Figure 7 Block diagram of the base-isolated system for the fuzzy controller

minus10 minus05 00 05 100

1PL

PMPSZENSNM

Deg

ree o

f mem

bers

hip

Normalized displacement

NL

00 05 100

1PL

PMPSZENSNM

Deg

ree o

f mem

bers

hip

Normalized velocity

NL

0 200 400 600 800 10000

1VL

LMS

Deg

ree o

f mem

bers

hip

Voltage (V)

ZE

minus10 minus05

Figure 8 Input and output membership functions of sublevel fuzzy control

variables are as follows NL negative large NM negativemedium NS negative small ZE zero PS positive small PMpositive medium and PL positive large The definition ofthe membership function of output variable is as follows ZEzero S small M medium L large and VL very large Themembership functions are employed Gaussian type for inputand output variables The fuzzy control rules are defined inTable 4

In the establishment of fuzzy control rules it followsthe following principles if the isolation displacement andvelocity are in opposite sign then the output voltage becomessmall in order to ensure output small damping force inthe piezoelectric friction damper Contrarily if the isolationdisplacement and velocity have the same sign the outputvoltage becomes large Certainly when the displacement andvelocity are almost zero or small the command voltage is

8 Mathematical Problems in Engineering

Table 4 Fuzzy control rules adopted for sublevel fuzzy control

Velocity ofisolated floor

Displacement of isolated floorNL NM NS ZE PS PM PL

NL VL VL L L M S ZENM VL L L M S ZE SNS L L M S ZE S MZE L M S ZE S M LPS M S ZE S M L LPM S ZE S M L L VLPL ZE S M L L VL VL

minus1minus05

005

1

minus1minus05

005

1

500

1000

VelocityDisplacement

Volta

ge (V

)

Figure 9 Fuzzy control surface for sublevel fuzzy controller

about zero this means that piezoelectric friction damper actsas a passive friction damper The defuzzification of fuzzycontrol adopts the method of centroid to get a crisp outputvalue The control surface and color-filled contour line ofsublevel fuzzy control are depicted in Figure 9

43 Supervisory Fuzzy Logic Controller In the fuzzy logiccontrol normalization factors need to satisfy a certain objec-tive The oversize normalization factors can enlarge the basedisplacement effectively Contrarily too small normalizationfactors can result in large control force that amplifies theaccelerations of base-isolated structure Thus a supervisoryfuzzy logic control is proposed to adjust its normalizationfactors in real-time As discussed earlier near-fault earth-quakes usually have long duration pulses with peak velocitiesThus the supervisory fuzzy control employs ground velocityas single input variable to identify the characteristics ofthe ground motion The normalization factors of sublevelfuzzy control are selected as two output variables HereGaussian membership functions are used for input andoutput variables as shown in

120583gauss = exp[minus(119909 minus 119888)2

21205902] (7)

where 119888 and 120590 are the constant values that define the shape ofthe Gauss functions respectively

The rules of the supervisory fuzzy controller are definedby the following form

Rule119894 IF 119883 is 119860119894 then 1198841is 1198621198941 1198842is 1198621198942

119894 = 1 2 119872

(8)

where119872 is the number of fuzzy control rules 119883 is the inputvariable 119884

1and 119884

2are the output variables 119860119894 119862119894

1 and 119862119894

2

are the linguistic values characterized by input and outputmembership functions respectively One fuzzy control ruleis described by three Gaussian membership functions andeach membership function can be defined by two parameters(119888 and 120590) Therefore a total of five fuzzy control rules canbe optimized by encoding these two parameters into thegene using genetic algorithm Consequently a total of 30parameters are encoded into the chromosome to define theinference system of supervisory fuzzy controller as shown inFigure 10

Similar to normalization factors the preload of thepiezoelectric friction dampers has a great influence on thedamping effect Thus it is essential to establish an effectivesupervisory fuzzy logic controller and a suitable preloadof piezoelectric friction damper Generally for the seismicprotection of a base-isolated structure there is a trade-off between the isolation displacement and superstructureacceleration The main control objective is to depress theisolation displacementwithout excessively increasing acceler-ation response of the superstructure In this section a geneticalgorithm is employed to seek out an optimal solution forthe control of the base-isolated structure The flow chart ofgenetic algorithm is shown in Figure 11

Genetic algorithm is a computational model for thesimulation of Darwin natural genetic selection and biologicalevolution Different from the traditional search algorithmgenetic algorithm begins to search a group of optimal solu-tions from an initial random population by mutation andrecombination Each individual which consists of a set ofbinary strings is a solution to the objective problem Afterinitialization genetic algorithm uses a sort method to rankindividuals It compares each solution with other solutionsin the population to find whether it is dominated Duringthe process of creating a new generation it selects a suitableindividual according to the size of the fitness value Afterseveral generations the individual value gradually convergesto the best chromosome which is the optimal solution

The objective fitness function employed in this study isshown as follows

119869 = 06 times119910119887max

119910119887max

+ 04 timesradicsum119899

119894=1(119886119894max119886119894max)

2

119899 (9)

where 119910119887max and 119910119887max denote the peak base displacements

for the fuzzy control and uncontrolled cases respectively119886119894max and 119886119894max represent the peak superstructure accelera-tion for the fuzzy control and uncontrolled case respectively

The objective of genetic algorithm is tomake the objectivefitness function reach its minimum value by selecting oneset of parameters of supervisory fuzzy control and preload

Mathematical Problems in Engineering 9

0

1

X

0

1

Deg

ree o

f mem

bers

hip

Deg

ree o

f mem

bers

hip

0

1

Deg

ree o

f mem

bers

hip

1205901

1205901 1205902 1205903

Rule 1 (1 6) Rule 1 (7 12) Rule 5 (24 30)middot middot middot

c1

c1 c2 c3

1205902

Y1

1205903

Y2c2 c3

Figure 10 Encoding structure for genetic algorithm

of piezoelectric friction damper The initial population sizegenetic algebra and crossover probability are set to 20 50and 08 respectively Through inputting the artificial earth-quakes which are characterized by near-fault earthquakesfor different ground sites the supervisory fuzzy control andpreload of piezoelectric friction dampers can be optimizedThe fuzzy control surfaces of optimized supervisory fuzzycontrol are shown in Figure 12

5 Linear Quadratic Gaussian Controller

LQG (Linear Quadratic Gaussian) method is based onKalman filter technique which has become a widely usedcontrol algorithm For comparison purpose LQG is adoptedto regulate the contact normal force of piezoelectric frictiondamper in the study The optimal controller takes groundacceleration as white noise and considers the velocity anddisplacement of base isolation as feedback signals Thecontrol performance index is defined as follows [22]

119869 = lim120591rarr+infin

1

120591

sdot 119864 int

120591

0

[Z (119905)119879QZ (119905) + U (119905)119879RU (119905)] 119889 (119905) (10)

where Q2119899times2119899

and R1times1

are semi-positive definite matrix andpositive definite matrix respectivelyThe control force can beobtained as follows

U (119905) = minusGZ (119905) (11)

G = Rminus1B119879P (12)

where P can be computed by the solution of the Riccatiequation as follows

minusPA minus A119879P + PBRminus1B119879P minusQ = 0 (13)

The control force obtained from the above equation isactive control force which could not be always achieved bypiezoelectric friction damper It is realized that the directionof active control force is opposite to the slipping direction ofpiezoelectric friction damper Therefore the desired controlforce119906

119889(119905) can be achieved according to the following criteria

119906119889(119905)

=

119891max sgn (119887) (119906active

119887lt 0

10038161003816100381610038161003816119906active10038161003816100381610038161003816 gt 119891max)

10038161003816100381610038161003816119906active10038161003816100381610038161003816 sgn (119887) (119906

active119887lt 0

10038161003816100381610038161003816119906active10038161003816100381610038161003816 le 119891max)

119891min sgn (119887) (119906active

119887ge 0)

(14)

10 Mathematical Problems in Engineering

Table 5 Parameters of base-isolated structure

Floor masses(kg)

Stiffness values(kNm)

Dampingcoefficients(kN sm)

Isolated floor 6800 232 745First floor 5897 33732 67Second floor 5897 29093 58Third floor 5897 28621 57Fourth floor 5897 24954 50Fifth floor 5897 19059 38

No

Yes

Encode

Generate initial random population

Calculate the value of fitness and rank

Copy crossover and mutation

Decode

Optimal solution

Whether or not to meet thecondition of convergence

Figure 11 Flow chart of genetic algorithm

where 119906active is the control force obtained from LQG con-troller

119887is the velocity of base isolator119891max and119891min are the

maximum and minimum friction forces of the piezoelectricfriction damper respectively

6 Numerical Simulations

61 Model of the Base-Isolated Structure A five-story base-isolated building which is proposed by He et al is employedto evaluate the performance of developed fuzzy controllers[18] The fundamental period of the five-story building is03 s For the given isolation parameters the fundamentalperiod of the base-isolated building becomes 25 sThereforean isolation ratio 120575 equal to 83 (=2503) is obtainedThe model of the base-isolated structure with piezoelectricfriction damper is shown in Figure 13 The parameters of thebase-isolated structure are shown in Table 5

62 Performance Evaluation Index In order to evaluate theperformance of base-isolated structure for different controlalgorithms a total of nine performance indexes are employedin this study [23] as shown in Table 6

The performance indexes J1through J

5denote the struc-

ture responses for the controlled building normalized byuncontrolled structure respectively The performance indexJ6evaluates the peak control force normalized by the peak

base shear for controlled structure The performance indexesJ7and J8represent RMS (Root Mean Square) base displace-

ments and RMS floor accelerations respectively J9computes

the energy dissipated by friction dampers normalized by theearthquake input energy to the controlled structure

63 Simulation Results and Analysis A total of nine seis-mic excitations that contain six real ground motions andthree artificial earthquakes are selected to evaluate the per-formance of the optimized fuzzy logic controller In thisstudy the time histories of strong earthquake which rangefrom 20 s to 70 s are selected for numerical simulation andanalysis

The numerical results for various earthquakes are listedin Table 7 In the table the Genetic Algorithm HierarchicFuzzy Logic Control is named as GHFLC Moreover forcomparison purpose the results for an optimal controller andpassive operation of friction damper are also listed in thetable Numbers in bold font indicate the best results amongall control cases

Base displacement is an important index to evaluatethe effectiveness for different controllers For a base-isolatedstructure the reduction of base displacement is a primarypurpose to prevent permanent damage for isolation bearingsor adjacent buildings Although passive operation of frictiondampers can successfully reduce the performance indexassociated with the peak and RMS base displacements (J

3and

J7) it causes significant amplification in peak and RMS floor

accelerations (J5and J

8) for most cases due to the passive

control For example as compared to the uncontrolledstructure for TCU052 TCU053 and TCU054 earthquakespassive control leads to 6 45 and 42 amplification inpeak floor acceleration respectively However the proposedfuzzy controller can successfully improve the base-isolatedstructure acceleration at the cost of slight deterioration in theperformance indices J

3and J7on comparison with passive

control For example for TCU052 TCU053 and TCU054earthquakes GHFLC results in 15 13 and 16 decrease inpeak floor accelerations respectively As compared to passivecontrol there are 9 3 and 7 increase in peak basedisplacements

The time histories of friction force and force-displacement curves of friction dampers for differentcontrollers subjected to TCU052 earthquake are shown inFigure 14 From the figures it can be seen that the passivecontrol outputs lager damper force than GHFLC Becausethe supervisory fuzzy control can alter input normalizationfactors of sublevel FLC according to the current level ofground motion there are some serrations presented at theedge of the hysteretic curve of piezoelectric friction damper

The comparison of the performance indexes J3 J7 J5and

J8under different control cases is shown in Figures 15 and

16 respectively From these figures it can be seen that thefuzzy controller is more effective than passive and optimal

Mathematical Problems in Engineering 11O

utpu

t

009

055

026

000033

000094000

Input ground velocity (ms)

Nd

N

(a) Hard soilO

utpu

t

Input ground velocity (ms)

071

042

000

008000

037

103000

Nd

N

(b) Medium soil

Out

put

Input ground velocity (ms)

107

053

000045

011000

117000

Nd

N

(c) Soft soil

Figure 12 Control surface for optimized supervisory fuzzy control

PFD

Fixed reference

LRB

Figure 13 Model of the base-isolated structure

12 Mathematical Problems in Engineering

Table 6 Performance index

Peak base shear Peak interstory drift RMS base displacement

1198691=max119905

10038171003817100381710038171198810 (119905)1003817100381710038171003817

max119905

100381710038171003817100381710038171198810(119905)10038171003817100381710038171003817

1198694=

max119905119891

10038171003817100381710038171003817119889119891(119905)10038171003817100381710038171003817

max119905119891

10038171003817100381710038171003817119889119891(119905)10038171003817100381710038171003817

1198697=

max119894

1003817100381710038171003817120590119889 (119905)1003817100381710038171003817

max119905

1003817100381710038171003817119889 (119905)1003817100381710038171003817

Peak structural shear Peak floor acceleration RMS floor acceleration

1198692=max119905

10038171003817100381710038171198811 (119905)1003817100381710038171003817

max119905

100381710038171003817100381710038171198811(119905)10038171003817100381710038171003817

1198695=

max119905119891

10038171003817100381710038171003817119886119891(119905)10038171003817100381710038171003817

max119905119891

10038171003817100381710038171003817119886119891(119905)10038171003817100381710038171003817

1198698=max119891

1003817100381710038171003817120590119886 (119905)1003817100381710038171003817

max119891

1003817100381710038171003817119886 (119905)1003817100381710038171003817

Peak base displacement Peak control force Energy dissipated by PFD

1198693=max119905

1003817100381710038171003817119909119887 (119905)1003817100381710038171003817

max119905

1003817100381710038171003817119909119887 (119905)1003817100381710038171003817

1198696=max119905

1003817100381710038171003817119891119889 (119905)1003817100381710038171003817

max119905

10038171003817100381710038171198810 (119905)1003817100381710038171003817

1198699=

int119879

0

119891119889(119905) 119887(119905) 119889119905

int119879

0

1198810(119905) 119892(119905) 119889119905

Table 7 Results of numerical simulation

Earthquake Control case 1198691

1198692

1198693

1198694

1198695

1198696

1198697

1198698

1198699

TCU102(hard site)

Passive 081 082 068 085 094 048 057 082 078Optimal 092 095 075 099 087 043 068 081 069GHFLC 087 091 071 093 082 041 061 078 073

TCU052(hard site)

Passive 079 079 046 082 106 036 038 089 087Optimal 087 087 057 087 098 029 049 085 079GHFLC 083 082 055 082 091 033 044 079 084

Artificialearthquake(hard site)

Passive 072 074 054 076 092 054 049 090 084Optimal 084 086 069 083 089 047 057 086 073GHFLC 076 077 061 079 083 042 052 081 076

TCU053(medium site)

Passive 061 065 039 071 145 032 037 116 089Optimal 069 072 046 076 136 031 045 117 078GHFLC 062 062 042 065 132 026 044 109 072

TCU054(medium site)

Passive 071 073 043 073 142 084 038 121 088Optimal 081 087 045 085 132 079 052 125 086GHFLC 075 071 040 074 126 082 045 113 076

Artificialearthquake(medium site)

Passive 054 057 038 064 123 067 036 117 091Optimal 067 066 047 067 119 078 048 113 079GHFLC 058 061 040 062 113 072 041 109 085

TCU110(soft soil site)

Passive 077 078 047 077 103 050 045 089 095Optimal 083 082 052 085 107 046 052 099 087GHFLC 086 086 056 086 104 042 049 093 090

CHY101(soft soil site)

Passive 069 071 058 075 086 066 054 092 084Optimal 075 073 062 074 087 064 055 088 079GHFLC 063 067 054 067 079 065 051 087 083

Artificialearthquake(soft site)

Passive 057 064 061 068 097 061 058 098 088Optimal 071 070 074 075 094 058 071 093 083GHFLC 065 062 067 069 085 055 063 086 076

controller in simultaneously depressing the superstructureacceleration and base displacement For example the appli-cation of developed fuzzy controller leads to an average of112 decrease in peak floor acceleration and an average ofonly 36 increase in peak base displacement as compared topassive control Particularly optimal controller produces anaverage of only 41 reduction in peak floor acceleration and

leads to 79 increase in peak base displacement as comparedto passive control Therefore the improved fuzzy controlmethod shows better performance than passive and optimalcontrol

In order to further evaluate the performance of differentcontrollers the energy time histories for different controllersare compared with each other For a base-isolated structure

Mathematical Problems in Engineering 13

20 30 40 50 60 70minus20

minus10

00

10

20Fr

ictio

n fo

rce (

kN)

Time (s)minus03 minus02 minus01 00 01 02 03

minus20

minus10

00

10

20

Fric

tion

forc

e (kN

)

Displacement (m)

(a) Passive control

20 30 40 50 60 70minus20

minus10

00

10

20

Fric

tion

forc

e (kN

)

Time (s)minus03 minus02 minus01 00 01 02 03

minus20

minus10

00

10

20

Fric

tion

forc

e (kN

)

Displacement (m)

(b) GHFLC method

Figure 14 Time histories of friction force and force-displacement diagram against TCU052 earthquake

1 2 3 4 5 6 7 8 903

04

05

06

07

08

Excitation case

Passive OptimalGHFLC

1 2 3 4 5 6 7 8 903

04

05

06

07

Excitation casePassive

GHFLC Optimal

J 3 J 5

Figure 15 Comparisons on the performance indexes J3and J7for different control cases

14 Mathematical Problems in Engineering

1 2 3 4 5 6 7 8 907

08

09

10

11

12

13

14

15

Excitation casePassive

GHFLC Optimal

1 2 3 4 5 6 7 8 907

08

09

10

11

12

13

Excitation case

Passive

GHFLC Optimal

J 8J 5

Figure 16 Comparison of the performance indexes J5and J8for different control cases

with piezoelectric friction dampers installed on the isolationthe energy equations are defined as follows

119864119870+ 119864120585+ 119864119878+ 119864119867= 119864119868

119864119870=1

2119879

119905119872119905

119864120585= int

119905

0

119879

119888 119889119905

119864119878= int

119905

0

119909119879

119870119889119909

119864119867= minusint

119905

0

119906119879

119864119879

119904119889119909

119864119868= minusint

119905

0

gMI 119889119909

(15)

where 119864119870 119864120585 119864119878 119864119867 and 119864

119868denote the absolute kinetic

energy damping energy elastic strain energy energy dis-sipated by piezoelectric friction dampers and total inputenergy respectively The energy time histories for differentcontrollers against TCU052Chi-Chi earthquake are shown inFigure 17 It can be seen from the figures that the piezoelectricfriction dampers dissipate most of the input energy fordifferent control cases subjected to TCU052 earthquake

In order to compare different effects under near-faultground motions recorded for different sites the average ofinput energy and structure responses subjected to near-faultearthquakes are given in Table 8

As shown in Table 8 the near-fault earthquakes forsoft sites are more destructive than hard sites For instancecompared to hard sites the input energy and the base dis-placement of RMS of the base-isolated structure for soft soil

increase by 143 and 256 respectively However GHFLCpossesses favorable performance under different ground sitesand the damping effect has no distinctly direct relationshipwith site category

As discussed in Section 61 the isolation ratio of thesimulation model equals 83 In order to evaluate the effectsof isolation ratio on the damping performance of GHFLC thestiffness value of isolation is adjusted to 1045 and 452 kNmrespectively Then the numerical results for different valuesof isolation ratio (120575 = 4 6) are obtained The performanceindexes J

3and J5for different isolation ratios are shown in

Figures 18 and 19 respectivelyFor base-isolated structure isolation ratio has a signifi-

cant influence on the isolation effect A larger isolation ratiowhich means a minor stiffness value of isolation usuallyleads to conspicuous enlargement of base displacement anddecrease of superstructural responses due to the increaseof fundamental vibration period and vice versa Howeveras shown in Figures 18 and 19 the shock absorption rateof GHFLC has little change when isolation ratio variesdifferently and the proposed fuzzy control shows favorableeffectiveness in the diverse isolation ratios of base-isolatedstructures

7 Conclusions

In this study an optimized fuzzy logic control which isdesigned for Chi-Chi near-fault earthquakes under differentground sites is proposed An elastic design spectrum isproposed to generate near-fault earthquakes for differentground sitesThe characteristic of the design spectrum is thatit has larger periods and peak acceleration than conventionalspectrum Genetic algorithm is employed to optimize thesupervisory fuzzy controller and preload of piezoelectric

Mathematical Problems in Engineering 15

Table 8 Average ofinput energy and structure responses subjected to near-fault earthquakes

Site classification Input energy (kNsdotm) Base shear (kN) Base displacement ofRMS (m)

Structure accelerationof RMS (g)

Hard soil 24375 475 0047 0432Medium soil 26746 498 0054 0476Soft soil 27857 568 0059 0531

20 30 40 50 60 7000

05

10

15

20

25

Input energyEnergy dissipated by dampers

Time (s)

Ener

gy (k

Nmiddotm

)

times104

(a) Passive control

20 30 40 50 60 7000

05

10

15

20

25

30

Time (s)

Input energyEnergy dissipated by dampers

Ener

gy (k

Nmiddotm

)

times104

(b) Optimal control

20 30 40 50 60 7000

05

10

15

20

25

30

Input energyEnergy dissipated by dampers

Time (s)

Ener

gy (k

Nmiddotm

)

times104

(c) GHFLC method

Figure 17 Energy time histories subjected to Chi-Chi TCU052 earthquake

friction dampers according to three artificial earthquakesthat are characterized by Chi-Chi earthquakes Passive andoptimal controllers are also compared with the performanceof the developed fuzzy controller The simulation resultsreveal that the developed semiactive fuzzy controller hasbetter performance than traditional passive and optimal con-troller in simultaneously reducing the base displacement and

floor acceleration under near-fault earthquakes for differentground sites

Conflict of Interests

The authors declare no conflict of interests regarding thepublication of this paper

16 Mathematical Problems in Engineering

1 2 3 4 5 6 7 8 903

04

05

06

07

08

Excitation casePassive

GHFLC Optimal

1 2 3 4 5 6 7 8 907

08

09

10

11

12

13

14

15

Excitation case

Passive

GHFLC Optimal

J 3 J 5Figure 18 Comparisons on the performance indexes J

3and J5for different control cases (120575 = 4)

1 2 3 4 5 6 7 8 903

04

05

06

07

08

Excitation casePassive

GHFLC Optimal

1 2 3 4 5 6 7 8 907

08

09

10

11

12

13

14

15

Excitation casePassive

GHFLC Optimal

J 3 J 5

Figure 19 Comparisons on the performance indexes J3and J5for different control cases (120575 = 6)

Acknowledgments

This research was supported by National Natural ScienceFoundation of China under Grant no 51308487 no 41402261and no 51408526 Hebei Provincial Natural Science Founda-tion ofChina underGrant no E2014203055 and the ExcellentYouth Foundation of Hebei Educational Committee underGrant no YQ2013015 The support for this research is greatlyappreciated

References

[1] C Alhan and H Gavin ldquoA parametric study of linear and non-linear passively damped seismic isolation systems for buildingsrdquoEngineering Structures vol 26 no 4 pp 485ndash497 2004

[2] R S Jangid and J M Kelly ldquoBase isolation for near-faultmotionsrdquoEarthquake Engineering and Structural Dynamics vol30 no 5 pp 691ndash707 2001

[3] J Shen M-H Tsai K-C Chang and G C Lee ldquoPerformanceof a seismically isolated bridge under near-fault earthquake

Mathematical Problems in Engineering 17

ground motionsrdquo Journal of Structural Engineering vol 130 no6 pp 861ndash868 2004

[4] F Mazza A Vulcano and M Mazza ldquoNonlinear dynamicresponse of RC buildings with different base Isolation systemssubjected to horizontal and vertical components of near-faultground motionsrdquo Open Construction and Building TechnologyJournal vol 6 pp 373ndash383 2012

[5] F Mazza and A Vulcano ldquoEffects of near-fault ground motionson the nonlinear dynamic response of base-isolated rc framedbuildingsrdquo Earthquake Engineering and Structural Dynamicsvol 41 no 2 pp 211ndash232 2012

[6] O E Ozbulut and S Hurlebaus ldquoFuzzy control of piezoelectricfriction dampers for seismic protection of smart base isolatedbuildingsrdquo Bulletin of Earthquake Engineering vol 8 no 6 pp1435ndash1455 2010

[7] O E Ozbulut M Bitaraf and S Hurlebaus ldquoAdaptive controlof base-isolated structures against near-field earthquakes usingvariable friction dampersrdquo Engineering Structures vol 33 no12 pp 3143ndash3154 2011

[8] J M Kelly ldquoThe role of damping in seismic isolationrdquo Earth-quake Engineering and Structural Dynamics vol 28 no 1 pp3ndash20 1999

[9] F Mazza and A Vulcano ldquoNonlinear response of RC framedbuildings with isolation and supplemental damping at the basesubjected to near-fault earthquakesrdquo Journal of EarthquakeEngineering vol 13 no 5 pp 690ndash715 2009

[10] M Bitaraf and S Hurlebaus ldquoSemi-active adaptive control ofseismically excited 20-story nonlinear buildingrdquo EngineeringStructures vol 56 no 11 pp 2107ndash2118 2013

[11] D Das T K Datta and A Madan ldquoSemiactive fuzzy controlof the seismic response of building frames with MR dampersrdquoEarthquake Engineering and Structural Dynamics vol 41 no 1pp 99ndash118 2012

[12] A-P Wang and C-D Lee ldquoFuzzy sliding mode control for abuilding structure based on genetic algorithmsrdquo EarthquakeEngineering and Structural Dynamics vol 31 no 4 pp 881ndash8952002

[13] D G Reigles and M D Symans ldquoSupervisory fuzzy controlof a base-isolated benchmark building utilizing a neuro-fuzzymodel of controllable fluid viscous dampersrdquo Structural Controland Health Monitoring vol 13 no 2-3 pp 724ndash747 2006

[14] H-S Kim and P N Roschke ldquoGA-fuzzy control of smartbase isolated benchmark building using supervisory controltechniquerdquo Advances in Engineering Software vol 38 no 7 pp453ndash465 2007

[15] D Yang and Y Zhao ldquoEffects of rupture forward directivity andfling step of near-fault groundmotions on seismic performanceof base-isolated building structurerdquo Acta Seismologica Sinicavol 32 no 5 pp 579ndash587 2010

[16] Y E-A Mohamedzein J A Abdalla and A Abdelwahab ldquoSiteresponse and earthquake design spectra for central KhartoumSudanrdquoBulletin of Earthquake Engineering vol 4 no 3 pp 277ndash293 2006

[17] D Zhao and H Li ldquoShaking table tests and analyses of semi-active fuzzy control for structural seismic reduction with apiezoelectric variable-friction damperrdquo Smart Materials andStructures vol 19 no 10 Article ID 105031 2010

[18] W L He A K Agrawal and J N Yang ldquoNovel semiactivefriction controller for linear structures against earthquakesrdquoJournal of Structural Engineering vol 129 no 7 pp 941ndash9502003

[19] J N Yang and A K Agrawal ldquoSemi-active hybrid controlsystems for nonlinear buildings against near-field earthquakesrdquoEngineering Structures vol 24 no 3 pp 271ndash280 2002

[20] O E Ozbulut and S Hurlebaus ldquoOptimal design of supere-lastic-friction base isolators for seismic protection of highwaybridges against near-field earthquakesrdquo Earthquake Engineeringand Structural Dynamics vol 40 no 3 pp 273ndash291 2011

[21] D A Shook P N Roschke and O E Ozbulut ldquoSuperelasticsemi-active damping of a base-isolated structurerdquo StructuralControl and HealthMonitoring vol 15 no 5 pp 746ndash768 2008

[22] K D PhamG JinM K Sain B F Spencer Jr and S R LibertyldquoGeneralized linear quadratic Gaussian techniques for the windbenchmark problemrdquo Journal of Engineering Mechanics vol130 no 4 pp 466ndash470 2004

[23] S Nagarajaiah and S Narasimhan ldquoSmart base-isolated bench-mark building Part II Phase I sample controllers for linearisolation systemsrdquo Structural Control and Health Monitoringvol 13 no 2-3 pp 605ndash625 2006

Submit your manuscripts athttpwwwhindawicom

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Mathematical Problems in Engineering

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Stochastic AnalysisInternational Journal of

Mathematical Problems in Engineering 5

0 2 4 6 8 10 12 14 16 18 20

minus03

minus02

minus01

00

01

02

03

Acce

lera

tion

(g)

Time (s)

(a) Time history of acceleration

0 2 4 6 8 10 12 14 16 18 20

minus09

minus06

minus03

00

03

06

09

Velo

city

(ms

)

Time (s)

(b) Time history of velocity

Figure 4 Artificial earthquakes for hard soil site

0 2 4 6 8 10 12 14 16 18 20

minus03

minus02

minus01

00

01

02

03

Acce

lera

tion

(g)

Time (s)

(a) Time history of acceleration

0 2 4 6 8 10 12 14 16 18 20

minus09

minus06

minus03

00

03

06

09Ve

loci

ty (m

s)

Time (s)

(b) Time history of velocity

Figure 5 Artificial earthquake for medium soil site

0 2 4 6 8 10 12 14 16 18 20

minus03

minus02

minus01

00

01

02

03

Acce

lera

tion

(g)

Time (s)

(a) Time history of acceleration

0 2 4 6 8 10 12 14 16 18 20

minus09

minus06

minus03

00

03

06

09

Velo

city

(ms

)

Time (s)

(b) Time history of velocity

Figure 6 Artificial earthquake for soft soil site

6 Mathematical Problems in Engineering

the time history of the generated artificial earthquakes for softsoil is distinct with the other Particularly the peak velocityreaches 09ms which is significantly greater than the other

3 Model of Base-Isolated Structure andPiezoelectric Friction Damper

31 Equation of Motion for Base-Isolated Structure Consideran n-degree of freedom base-isolated structure with a piezo-electric friction damper at the isolation floor the dynamicequation of the base-isolated system is given by

MX (119905) + CX (119905) + KX (119905) = B119904U (119905) + E

119904119892(119905) (2)

where M C and K represent 119899 times 119899 mass damping andstiffness matrices respectively X(119905) X(119905) and X(119905) are theacceleration velocity and displacement vectors respectivelyU(119905) is the control force generated by the piezoelectric frictiondamper and

119892(119905) is the earthquake acceleration

Rewriting (2) in state-space form gives

Z (119905) = AZ (119905) + BU (119905) + E119892(119905) (3)

where

Z (119905) = [X (119905)X (119905)

]

E = [0119899times1

Mminus1E119904

]

B = [0119899times1

Mminus1B119904

]

A = [0119899times119899

I119899times119899

minusMminus1K minusMminus1C]

(4)

32 Model of Piezoelectric Friction Damper Piezoelectricfriction damper is a novel semiactive control device whichutilizes piezoelectric stacks to regulate the damping forceto provide a satisfying level of friction force Recently theauthors also proposed a piezoelectric friction damper andinvestigated their performances theoretically and experimen-tally [17]

During the movement of the base-isolated structure afriction damper has two possible motion states sticking andslipping phases [18 19] The friction force of the piezoelectricfriction damper is given as [20]

119873(119905) = 119873pre + 119862pz119881 (119905)

119891 (119905) = minus120583119873 (119905) sgn () = 0

minus120583119873 (119905) le 119891 (119905) le 120583119873 (119905) = 0

(5)

where 119873(119905) is the total contact force 119873pre represents thepreload of the piezoelectric friction damper 119862pz is thepiezoelectric coefficient of the piezoelectric actuator 119881(119905)is the input voltage of piezoelectric stack actuator 120583 is the

Table 3 Parameters of piezoelectric friction damper

Parameters Values120583 04119862pz 1125NV119881max 1000V

friction coefficient of the damper sgn(sdot) represents the signfunction related to the slip rate of the damper and 119891(119905)denotes damping force of piezoelectric friction damper

However the static state of the piezoelectric frictiondamper is complex to be estimated Shook et al [21] proposedan approximate calculation formula for the sticking frictionforce as given in the following

119891119904= minus120583119873 (119905) sgn ()

when 119891119904=1003816100381610038161003816119891119894 + 119891119903

1003816100381610038161003816 1003816100381610038161003816119891 (119905)

1003816100381610038161003816 ge 119891119904

119891119894= 119898119905119892= (119898

119887+

119899

sum

119894=1

119898119894) 119892

119891119903= 119896119887119909119887

(6)

where 119891119894is the inertial force applied on the mass 119891

119903is the

restoring force provided by the isolation bearing 119898119894is the

mass of the superstructure 119898119887and 119896

119887are the mass and

stiffness of base isolator and 119909119887is the displacement of base

isolatorThe parameters of piezoelectric friction damper are listed

in Table 3 And the preload of the piezoelectric frictiondamper can be optimized by genetic algorithm

4 GA-Based Hierarchic Fuzzy ControlAlgorithm

41 Framework of the Developed Fuzzy Logic Controller Thecontroller adopts a hierarchic fuzzy control algorithm inwhich a supervisory fuzzy controller governs a sublevelfuzzy controller by altering its input normalization factorsaccording to the current level of groundmotionThe sublevelfuzzy logic controller is designed to determine the commandvoltage of piezoelectric friction damper according to thevelocity and displacement of base isolation Piezoelectricfriction damper regulates the damping force according tothe input voltage Genetic algorithm is employed to optimizesupervisory fuzzy controller and preload of piezoelectricfriction damper according to an objective function and thegenerated artificial earthquakes for different ground sitesTheblock diagram of the system for the developed controller isshown in Figure 7

42 Sublevel Fuzzy Controller The sublevel fuzzy controlleris established in order to determine the command voltage ofthe piezoelectric friction damper The isolation displacementand velocity are selected as two input variables and commandvoltage is employed as a single output variable as shown inFigure 8The definitions of themembership function of input

Mathematical Problems in Engineering 7

Ground motion

Damping force

Semiactiveisolated

structure

Piezoelectricfriction damper

Ground velocity

Optimize

Voltage

Structural response

Isolation velocity and displacement

Sublevel fuzzycontroller

Supervisoryfuzzy controller

Optimize

Genetic algorithm

Nd

N

Figure 7 Block diagram of the base-isolated system for the fuzzy controller

minus10 minus05 00 05 100

1PL

PMPSZENSNM

Deg

ree o

f mem

bers

hip

Normalized displacement

NL

00 05 100

1PL

PMPSZENSNM

Deg

ree o

f mem

bers

hip

Normalized velocity

NL

0 200 400 600 800 10000

1VL

LMS

Deg

ree o

f mem

bers

hip

Voltage (V)

ZE

minus10 minus05

Figure 8 Input and output membership functions of sublevel fuzzy control

variables are as follows NL negative large NM negativemedium NS negative small ZE zero PS positive small PMpositive medium and PL positive large The definition ofthe membership function of output variable is as follows ZEzero S small M medium L large and VL very large Themembership functions are employed Gaussian type for inputand output variables The fuzzy control rules are defined inTable 4

In the establishment of fuzzy control rules it followsthe following principles if the isolation displacement andvelocity are in opposite sign then the output voltage becomessmall in order to ensure output small damping force inthe piezoelectric friction damper Contrarily if the isolationdisplacement and velocity have the same sign the outputvoltage becomes large Certainly when the displacement andvelocity are almost zero or small the command voltage is

8 Mathematical Problems in Engineering

Table 4 Fuzzy control rules adopted for sublevel fuzzy control

Velocity ofisolated floor

Displacement of isolated floorNL NM NS ZE PS PM PL

NL VL VL L L M S ZENM VL L L M S ZE SNS L L M S ZE S MZE L M S ZE S M LPS M S ZE S M L LPM S ZE S M L L VLPL ZE S M L L VL VL

minus1minus05

005

1

minus1minus05

005

1

500

1000

VelocityDisplacement

Volta

ge (V

)

Figure 9 Fuzzy control surface for sublevel fuzzy controller

about zero this means that piezoelectric friction damper actsas a passive friction damper The defuzzification of fuzzycontrol adopts the method of centroid to get a crisp outputvalue The control surface and color-filled contour line ofsublevel fuzzy control are depicted in Figure 9

43 Supervisory Fuzzy Logic Controller In the fuzzy logiccontrol normalization factors need to satisfy a certain objec-tive The oversize normalization factors can enlarge the basedisplacement effectively Contrarily too small normalizationfactors can result in large control force that amplifies theaccelerations of base-isolated structure Thus a supervisoryfuzzy logic control is proposed to adjust its normalizationfactors in real-time As discussed earlier near-fault earth-quakes usually have long duration pulses with peak velocitiesThus the supervisory fuzzy control employs ground velocityas single input variable to identify the characteristics ofthe ground motion The normalization factors of sublevelfuzzy control are selected as two output variables HereGaussian membership functions are used for input andoutput variables as shown in

120583gauss = exp[minus(119909 minus 119888)2

21205902] (7)

where 119888 and 120590 are the constant values that define the shape ofthe Gauss functions respectively

The rules of the supervisory fuzzy controller are definedby the following form

Rule119894 IF 119883 is 119860119894 then 1198841is 1198621198941 1198842is 1198621198942

119894 = 1 2 119872

(8)

where119872 is the number of fuzzy control rules 119883 is the inputvariable 119884

1and 119884

2are the output variables 119860119894 119862119894

1 and 119862119894

2

are the linguistic values characterized by input and outputmembership functions respectively One fuzzy control ruleis described by three Gaussian membership functions andeach membership function can be defined by two parameters(119888 and 120590) Therefore a total of five fuzzy control rules canbe optimized by encoding these two parameters into thegene using genetic algorithm Consequently a total of 30parameters are encoded into the chromosome to define theinference system of supervisory fuzzy controller as shown inFigure 10

Similar to normalization factors the preload of thepiezoelectric friction dampers has a great influence on thedamping effect Thus it is essential to establish an effectivesupervisory fuzzy logic controller and a suitable preloadof piezoelectric friction damper Generally for the seismicprotection of a base-isolated structure there is a trade-off between the isolation displacement and superstructureacceleration The main control objective is to depress theisolation displacementwithout excessively increasing acceler-ation response of the superstructure In this section a geneticalgorithm is employed to seek out an optimal solution forthe control of the base-isolated structure The flow chart ofgenetic algorithm is shown in Figure 11

Genetic algorithm is a computational model for thesimulation of Darwin natural genetic selection and biologicalevolution Different from the traditional search algorithmgenetic algorithm begins to search a group of optimal solu-tions from an initial random population by mutation andrecombination Each individual which consists of a set ofbinary strings is a solution to the objective problem Afterinitialization genetic algorithm uses a sort method to rankindividuals It compares each solution with other solutionsin the population to find whether it is dominated Duringthe process of creating a new generation it selects a suitableindividual according to the size of the fitness value Afterseveral generations the individual value gradually convergesto the best chromosome which is the optimal solution

The objective fitness function employed in this study isshown as follows

119869 = 06 times119910119887max

119910119887max

+ 04 timesradicsum119899

119894=1(119886119894max119886119894max)

2

119899 (9)

where 119910119887max and 119910119887max denote the peak base displacements

for the fuzzy control and uncontrolled cases respectively119886119894max and 119886119894max represent the peak superstructure accelera-tion for the fuzzy control and uncontrolled case respectively

The objective of genetic algorithm is tomake the objectivefitness function reach its minimum value by selecting oneset of parameters of supervisory fuzzy control and preload

Mathematical Problems in Engineering 9

0

1

X

0

1

Deg

ree o

f mem

bers

hip

Deg

ree o

f mem

bers

hip

0

1

Deg

ree o

f mem

bers

hip

1205901

1205901 1205902 1205903

Rule 1 (1 6) Rule 1 (7 12) Rule 5 (24 30)middot middot middot

c1

c1 c2 c3

1205902

Y1

1205903

Y2c2 c3

Figure 10 Encoding structure for genetic algorithm

of piezoelectric friction damper The initial population sizegenetic algebra and crossover probability are set to 20 50and 08 respectively Through inputting the artificial earth-quakes which are characterized by near-fault earthquakesfor different ground sites the supervisory fuzzy control andpreload of piezoelectric friction dampers can be optimizedThe fuzzy control surfaces of optimized supervisory fuzzycontrol are shown in Figure 12

5 Linear Quadratic Gaussian Controller

LQG (Linear Quadratic Gaussian) method is based onKalman filter technique which has become a widely usedcontrol algorithm For comparison purpose LQG is adoptedto regulate the contact normal force of piezoelectric frictiondamper in the study The optimal controller takes groundacceleration as white noise and considers the velocity anddisplacement of base isolation as feedback signals Thecontrol performance index is defined as follows [22]

119869 = lim120591rarr+infin

1

120591

sdot 119864 int

120591

0

[Z (119905)119879QZ (119905) + U (119905)119879RU (119905)] 119889 (119905) (10)

where Q2119899times2119899

and R1times1

are semi-positive definite matrix andpositive definite matrix respectivelyThe control force can beobtained as follows

U (119905) = minusGZ (119905) (11)

G = Rminus1B119879P (12)

where P can be computed by the solution of the Riccatiequation as follows

minusPA minus A119879P + PBRminus1B119879P minusQ = 0 (13)

The control force obtained from the above equation isactive control force which could not be always achieved bypiezoelectric friction damper It is realized that the directionof active control force is opposite to the slipping direction ofpiezoelectric friction damper Therefore the desired controlforce119906

119889(119905) can be achieved according to the following criteria

119906119889(119905)

=

119891max sgn (119887) (119906active

119887lt 0

10038161003816100381610038161003816119906active10038161003816100381610038161003816 gt 119891max)

10038161003816100381610038161003816119906active10038161003816100381610038161003816 sgn (119887) (119906

active119887lt 0

10038161003816100381610038161003816119906active10038161003816100381610038161003816 le 119891max)

119891min sgn (119887) (119906active

119887ge 0)

(14)

10 Mathematical Problems in Engineering

Table 5 Parameters of base-isolated structure

Floor masses(kg)

Stiffness values(kNm)

Dampingcoefficients(kN sm)

Isolated floor 6800 232 745First floor 5897 33732 67Second floor 5897 29093 58Third floor 5897 28621 57Fourth floor 5897 24954 50Fifth floor 5897 19059 38

No

Yes

Encode

Generate initial random population

Calculate the value of fitness and rank

Copy crossover and mutation

Decode

Optimal solution

Whether or not to meet thecondition of convergence

Figure 11 Flow chart of genetic algorithm

where 119906active is the control force obtained from LQG con-troller

119887is the velocity of base isolator119891max and119891min are the

maximum and minimum friction forces of the piezoelectricfriction damper respectively

6 Numerical Simulations

61 Model of the Base-Isolated Structure A five-story base-isolated building which is proposed by He et al is employedto evaluate the performance of developed fuzzy controllers[18] The fundamental period of the five-story building is03 s For the given isolation parameters the fundamentalperiod of the base-isolated building becomes 25 sThereforean isolation ratio 120575 equal to 83 (=2503) is obtainedThe model of the base-isolated structure with piezoelectricfriction damper is shown in Figure 13 The parameters of thebase-isolated structure are shown in Table 5

62 Performance Evaluation Index In order to evaluate theperformance of base-isolated structure for different controlalgorithms a total of nine performance indexes are employedin this study [23] as shown in Table 6

The performance indexes J1through J

5denote the struc-

ture responses for the controlled building normalized byuncontrolled structure respectively The performance indexJ6evaluates the peak control force normalized by the peak

base shear for controlled structure The performance indexesJ7and J8represent RMS (Root Mean Square) base displace-

ments and RMS floor accelerations respectively J9computes

the energy dissipated by friction dampers normalized by theearthquake input energy to the controlled structure

63 Simulation Results and Analysis A total of nine seis-mic excitations that contain six real ground motions andthree artificial earthquakes are selected to evaluate the per-formance of the optimized fuzzy logic controller In thisstudy the time histories of strong earthquake which rangefrom 20 s to 70 s are selected for numerical simulation andanalysis

The numerical results for various earthquakes are listedin Table 7 In the table the Genetic Algorithm HierarchicFuzzy Logic Control is named as GHFLC Moreover forcomparison purpose the results for an optimal controller andpassive operation of friction damper are also listed in thetable Numbers in bold font indicate the best results amongall control cases

Base displacement is an important index to evaluatethe effectiveness for different controllers For a base-isolatedstructure the reduction of base displacement is a primarypurpose to prevent permanent damage for isolation bearingsor adjacent buildings Although passive operation of frictiondampers can successfully reduce the performance indexassociated with the peak and RMS base displacements (J

3and

J7) it causes significant amplification in peak and RMS floor

accelerations (J5and J

8) for most cases due to the passive

control For example as compared to the uncontrolledstructure for TCU052 TCU053 and TCU054 earthquakespassive control leads to 6 45 and 42 amplification inpeak floor acceleration respectively However the proposedfuzzy controller can successfully improve the base-isolatedstructure acceleration at the cost of slight deterioration in theperformance indices J

3and J7on comparison with passive

control For example for TCU052 TCU053 and TCU054earthquakes GHFLC results in 15 13 and 16 decrease inpeak floor accelerations respectively As compared to passivecontrol there are 9 3 and 7 increase in peak basedisplacements

The time histories of friction force and force-displacement curves of friction dampers for differentcontrollers subjected to TCU052 earthquake are shown inFigure 14 From the figures it can be seen that the passivecontrol outputs lager damper force than GHFLC Becausethe supervisory fuzzy control can alter input normalizationfactors of sublevel FLC according to the current level ofground motion there are some serrations presented at theedge of the hysteretic curve of piezoelectric friction damper

The comparison of the performance indexes J3 J7 J5and

J8under different control cases is shown in Figures 15 and

16 respectively From these figures it can be seen that thefuzzy controller is more effective than passive and optimal

Mathematical Problems in Engineering 11O

utpu

t

009

055

026

000033

000094000

Input ground velocity (ms)

Nd

N

(a) Hard soilO

utpu

t

Input ground velocity (ms)

071

042

000

008000

037

103000

Nd

N

(b) Medium soil

Out

put

Input ground velocity (ms)

107

053

000045

011000

117000

Nd

N

(c) Soft soil

Figure 12 Control surface for optimized supervisory fuzzy control

PFD

Fixed reference

LRB

Figure 13 Model of the base-isolated structure

12 Mathematical Problems in Engineering

Table 6 Performance index

Peak base shear Peak interstory drift RMS base displacement

1198691=max119905

10038171003817100381710038171198810 (119905)1003817100381710038171003817

max119905

100381710038171003817100381710038171198810(119905)10038171003817100381710038171003817

1198694=

max119905119891

10038171003817100381710038171003817119889119891(119905)10038171003817100381710038171003817

max119905119891

10038171003817100381710038171003817119889119891(119905)10038171003817100381710038171003817

1198697=

max119894

1003817100381710038171003817120590119889 (119905)1003817100381710038171003817

max119905

1003817100381710038171003817119889 (119905)1003817100381710038171003817

Peak structural shear Peak floor acceleration RMS floor acceleration

1198692=max119905

10038171003817100381710038171198811 (119905)1003817100381710038171003817

max119905

100381710038171003817100381710038171198811(119905)10038171003817100381710038171003817

1198695=

max119905119891

10038171003817100381710038171003817119886119891(119905)10038171003817100381710038171003817

max119905119891

10038171003817100381710038171003817119886119891(119905)10038171003817100381710038171003817

1198698=max119891

1003817100381710038171003817120590119886 (119905)1003817100381710038171003817

max119891

1003817100381710038171003817119886 (119905)1003817100381710038171003817

Peak base displacement Peak control force Energy dissipated by PFD

1198693=max119905

1003817100381710038171003817119909119887 (119905)1003817100381710038171003817

max119905

1003817100381710038171003817119909119887 (119905)1003817100381710038171003817

1198696=max119905

1003817100381710038171003817119891119889 (119905)1003817100381710038171003817

max119905

10038171003817100381710038171198810 (119905)1003817100381710038171003817

1198699=

int119879

0

119891119889(119905) 119887(119905) 119889119905

int119879

0

1198810(119905) 119892(119905) 119889119905

Table 7 Results of numerical simulation

Earthquake Control case 1198691

1198692

1198693

1198694

1198695

1198696

1198697

1198698

1198699

TCU102(hard site)

Passive 081 082 068 085 094 048 057 082 078Optimal 092 095 075 099 087 043 068 081 069GHFLC 087 091 071 093 082 041 061 078 073

TCU052(hard site)

Passive 079 079 046 082 106 036 038 089 087Optimal 087 087 057 087 098 029 049 085 079GHFLC 083 082 055 082 091 033 044 079 084

Artificialearthquake(hard site)

Passive 072 074 054 076 092 054 049 090 084Optimal 084 086 069 083 089 047 057 086 073GHFLC 076 077 061 079 083 042 052 081 076

TCU053(medium site)

Passive 061 065 039 071 145 032 037 116 089Optimal 069 072 046 076 136 031 045 117 078GHFLC 062 062 042 065 132 026 044 109 072

TCU054(medium site)

Passive 071 073 043 073 142 084 038 121 088Optimal 081 087 045 085 132 079 052 125 086GHFLC 075 071 040 074 126 082 045 113 076

Artificialearthquake(medium site)

Passive 054 057 038 064 123 067 036 117 091Optimal 067 066 047 067 119 078 048 113 079GHFLC 058 061 040 062 113 072 041 109 085

TCU110(soft soil site)

Passive 077 078 047 077 103 050 045 089 095Optimal 083 082 052 085 107 046 052 099 087GHFLC 086 086 056 086 104 042 049 093 090

CHY101(soft soil site)

Passive 069 071 058 075 086 066 054 092 084Optimal 075 073 062 074 087 064 055 088 079GHFLC 063 067 054 067 079 065 051 087 083

Artificialearthquake(soft site)

Passive 057 064 061 068 097 061 058 098 088Optimal 071 070 074 075 094 058 071 093 083GHFLC 065 062 067 069 085 055 063 086 076

controller in simultaneously depressing the superstructureacceleration and base displacement For example the appli-cation of developed fuzzy controller leads to an average of112 decrease in peak floor acceleration and an average ofonly 36 increase in peak base displacement as compared topassive control Particularly optimal controller produces anaverage of only 41 reduction in peak floor acceleration and

leads to 79 increase in peak base displacement as comparedto passive control Therefore the improved fuzzy controlmethod shows better performance than passive and optimalcontrol

In order to further evaluate the performance of differentcontrollers the energy time histories for different controllersare compared with each other For a base-isolated structure

Mathematical Problems in Engineering 13

20 30 40 50 60 70minus20

minus10

00

10

20Fr

ictio

n fo

rce (

kN)

Time (s)minus03 minus02 minus01 00 01 02 03

minus20

minus10

00

10

20

Fric

tion

forc

e (kN

)

Displacement (m)

(a) Passive control

20 30 40 50 60 70minus20

minus10

00

10

20

Fric

tion

forc

e (kN

)

Time (s)minus03 minus02 minus01 00 01 02 03

minus20

minus10

00

10

20

Fric

tion

forc

e (kN

)

Displacement (m)

(b) GHFLC method

Figure 14 Time histories of friction force and force-displacement diagram against TCU052 earthquake

1 2 3 4 5 6 7 8 903

04

05

06

07

08

Excitation case

Passive OptimalGHFLC

1 2 3 4 5 6 7 8 903

04

05

06

07

Excitation casePassive

GHFLC Optimal

J 3 J 5

Figure 15 Comparisons on the performance indexes J3and J7for different control cases

14 Mathematical Problems in Engineering

1 2 3 4 5 6 7 8 907

08

09

10

11

12

13

14

15

Excitation casePassive

GHFLC Optimal

1 2 3 4 5 6 7 8 907

08

09

10

11

12

13

Excitation case

Passive

GHFLC Optimal

J 8J 5

Figure 16 Comparison of the performance indexes J5and J8for different control cases

with piezoelectric friction dampers installed on the isolationthe energy equations are defined as follows

119864119870+ 119864120585+ 119864119878+ 119864119867= 119864119868

119864119870=1

2119879

119905119872119905

119864120585= int

119905

0

119879

119888 119889119905

119864119878= int

119905

0

119909119879

119870119889119909

119864119867= minusint

119905

0

119906119879

119864119879

119904119889119909

119864119868= minusint

119905

0

gMI 119889119909

(15)

where 119864119870 119864120585 119864119878 119864119867 and 119864

119868denote the absolute kinetic

energy damping energy elastic strain energy energy dis-sipated by piezoelectric friction dampers and total inputenergy respectively The energy time histories for differentcontrollers against TCU052Chi-Chi earthquake are shown inFigure 17 It can be seen from the figures that the piezoelectricfriction dampers dissipate most of the input energy fordifferent control cases subjected to TCU052 earthquake

In order to compare different effects under near-faultground motions recorded for different sites the average ofinput energy and structure responses subjected to near-faultearthquakes are given in Table 8

As shown in Table 8 the near-fault earthquakes forsoft sites are more destructive than hard sites For instancecompared to hard sites the input energy and the base dis-placement of RMS of the base-isolated structure for soft soil

increase by 143 and 256 respectively However GHFLCpossesses favorable performance under different ground sitesand the damping effect has no distinctly direct relationshipwith site category

As discussed in Section 61 the isolation ratio of thesimulation model equals 83 In order to evaluate the effectsof isolation ratio on the damping performance of GHFLC thestiffness value of isolation is adjusted to 1045 and 452 kNmrespectively Then the numerical results for different valuesof isolation ratio (120575 = 4 6) are obtained The performanceindexes J

3and J5for different isolation ratios are shown in

Figures 18 and 19 respectivelyFor base-isolated structure isolation ratio has a signifi-

cant influence on the isolation effect A larger isolation ratiowhich means a minor stiffness value of isolation usuallyleads to conspicuous enlargement of base displacement anddecrease of superstructural responses due to the increaseof fundamental vibration period and vice versa Howeveras shown in Figures 18 and 19 the shock absorption rateof GHFLC has little change when isolation ratio variesdifferently and the proposed fuzzy control shows favorableeffectiveness in the diverse isolation ratios of base-isolatedstructures

7 Conclusions

In this study an optimized fuzzy logic control which isdesigned for Chi-Chi near-fault earthquakes under differentground sites is proposed An elastic design spectrum isproposed to generate near-fault earthquakes for differentground sitesThe characteristic of the design spectrum is thatit has larger periods and peak acceleration than conventionalspectrum Genetic algorithm is employed to optimize thesupervisory fuzzy controller and preload of piezoelectric

Mathematical Problems in Engineering 15

Table 8 Average ofinput energy and structure responses subjected to near-fault earthquakes

Site classification Input energy (kNsdotm) Base shear (kN) Base displacement ofRMS (m)

Structure accelerationof RMS (g)

Hard soil 24375 475 0047 0432Medium soil 26746 498 0054 0476Soft soil 27857 568 0059 0531

20 30 40 50 60 7000

05

10

15

20

25

Input energyEnergy dissipated by dampers

Time (s)

Ener

gy (k

Nmiddotm

)

times104

(a) Passive control

20 30 40 50 60 7000

05

10

15

20

25

30

Time (s)

Input energyEnergy dissipated by dampers

Ener

gy (k

Nmiddotm

)

times104

(b) Optimal control

20 30 40 50 60 7000

05

10

15

20

25

30

Input energyEnergy dissipated by dampers

Time (s)

Ener

gy (k

Nmiddotm

)

times104

(c) GHFLC method

Figure 17 Energy time histories subjected to Chi-Chi TCU052 earthquake

friction dampers according to three artificial earthquakesthat are characterized by Chi-Chi earthquakes Passive andoptimal controllers are also compared with the performanceof the developed fuzzy controller The simulation resultsreveal that the developed semiactive fuzzy controller hasbetter performance than traditional passive and optimal con-troller in simultaneously reducing the base displacement and

floor acceleration under near-fault earthquakes for differentground sites

Conflict of Interests

The authors declare no conflict of interests regarding thepublication of this paper

16 Mathematical Problems in Engineering

1 2 3 4 5 6 7 8 903

04

05

06

07

08

Excitation casePassive

GHFLC Optimal

1 2 3 4 5 6 7 8 907

08

09

10

11

12

13

14

15

Excitation case

Passive

GHFLC Optimal

J 3 J 5Figure 18 Comparisons on the performance indexes J

3and J5for different control cases (120575 = 4)

1 2 3 4 5 6 7 8 903

04

05

06

07

08

Excitation casePassive

GHFLC Optimal

1 2 3 4 5 6 7 8 907

08

09

10

11

12

13

14

15

Excitation casePassive

GHFLC Optimal

J 3 J 5

Figure 19 Comparisons on the performance indexes J3and J5for different control cases (120575 = 6)

Acknowledgments

This research was supported by National Natural ScienceFoundation of China under Grant no 51308487 no 41402261and no 51408526 Hebei Provincial Natural Science Founda-tion ofChina underGrant no E2014203055 and the ExcellentYouth Foundation of Hebei Educational Committee underGrant no YQ2013015 The support for this research is greatlyappreciated

References

[1] C Alhan and H Gavin ldquoA parametric study of linear and non-linear passively damped seismic isolation systems for buildingsrdquoEngineering Structures vol 26 no 4 pp 485ndash497 2004

[2] R S Jangid and J M Kelly ldquoBase isolation for near-faultmotionsrdquoEarthquake Engineering and Structural Dynamics vol30 no 5 pp 691ndash707 2001

[3] J Shen M-H Tsai K-C Chang and G C Lee ldquoPerformanceof a seismically isolated bridge under near-fault earthquake

Mathematical Problems in Engineering 17

ground motionsrdquo Journal of Structural Engineering vol 130 no6 pp 861ndash868 2004

[4] F Mazza A Vulcano and M Mazza ldquoNonlinear dynamicresponse of RC buildings with different base Isolation systemssubjected to horizontal and vertical components of near-faultground motionsrdquo Open Construction and Building TechnologyJournal vol 6 pp 373ndash383 2012

[5] F Mazza and A Vulcano ldquoEffects of near-fault ground motionson the nonlinear dynamic response of base-isolated rc framedbuildingsrdquo Earthquake Engineering and Structural Dynamicsvol 41 no 2 pp 211ndash232 2012

[6] O E Ozbulut and S Hurlebaus ldquoFuzzy control of piezoelectricfriction dampers for seismic protection of smart base isolatedbuildingsrdquo Bulletin of Earthquake Engineering vol 8 no 6 pp1435ndash1455 2010

[7] O E Ozbulut M Bitaraf and S Hurlebaus ldquoAdaptive controlof base-isolated structures against near-field earthquakes usingvariable friction dampersrdquo Engineering Structures vol 33 no12 pp 3143ndash3154 2011

[8] J M Kelly ldquoThe role of damping in seismic isolationrdquo Earth-quake Engineering and Structural Dynamics vol 28 no 1 pp3ndash20 1999

[9] F Mazza and A Vulcano ldquoNonlinear response of RC framedbuildings with isolation and supplemental damping at the basesubjected to near-fault earthquakesrdquo Journal of EarthquakeEngineering vol 13 no 5 pp 690ndash715 2009

[10] M Bitaraf and S Hurlebaus ldquoSemi-active adaptive control ofseismically excited 20-story nonlinear buildingrdquo EngineeringStructures vol 56 no 11 pp 2107ndash2118 2013

[11] D Das T K Datta and A Madan ldquoSemiactive fuzzy controlof the seismic response of building frames with MR dampersrdquoEarthquake Engineering and Structural Dynamics vol 41 no 1pp 99ndash118 2012

[12] A-P Wang and C-D Lee ldquoFuzzy sliding mode control for abuilding structure based on genetic algorithmsrdquo EarthquakeEngineering and Structural Dynamics vol 31 no 4 pp 881ndash8952002

[13] D G Reigles and M D Symans ldquoSupervisory fuzzy controlof a base-isolated benchmark building utilizing a neuro-fuzzymodel of controllable fluid viscous dampersrdquo Structural Controland Health Monitoring vol 13 no 2-3 pp 724ndash747 2006

[14] H-S Kim and P N Roschke ldquoGA-fuzzy control of smartbase isolated benchmark building using supervisory controltechniquerdquo Advances in Engineering Software vol 38 no 7 pp453ndash465 2007

[15] D Yang and Y Zhao ldquoEffects of rupture forward directivity andfling step of near-fault groundmotions on seismic performanceof base-isolated building structurerdquo Acta Seismologica Sinicavol 32 no 5 pp 579ndash587 2010

[16] Y E-A Mohamedzein J A Abdalla and A Abdelwahab ldquoSiteresponse and earthquake design spectra for central KhartoumSudanrdquoBulletin of Earthquake Engineering vol 4 no 3 pp 277ndash293 2006

[17] D Zhao and H Li ldquoShaking table tests and analyses of semi-active fuzzy control for structural seismic reduction with apiezoelectric variable-friction damperrdquo Smart Materials andStructures vol 19 no 10 Article ID 105031 2010

[18] W L He A K Agrawal and J N Yang ldquoNovel semiactivefriction controller for linear structures against earthquakesrdquoJournal of Structural Engineering vol 129 no 7 pp 941ndash9502003

[19] J N Yang and A K Agrawal ldquoSemi-active hybrid controlsystems for nonlinear buildings against near-field earthquakesrdquoEngineering Structures vol 24 no 3 pp 271ndash280 2002

[20] O E Ozbulut and S Hurlebaus ldquoOptimal design of supere-lastic-friction base isolators for seismic protection of highwaybridges against near-field earthquakesrdquo Earthquake Engineeringand Structural Dynamics vol 40 no 3 pp 273ndash291 2011

[21] D A Shook P N Roschke and O E Ozbulut ldquoSuperelasticsemi-active damping of a base-isolated structurerdquo StructuralControl and HealthMonitoring vol 15 no 5 pp 746ndash768 2008

[22] K D PhamG JinM K Sain B F Spencer Jr and S R LibertyldquoGeneralized linear quadratic Gaussian techniques for the windbenchmark problemrdquo Journal of Engineering Mechanics vol130 no 4 pp 466ndash470 2004

[23] S Nagarajaiah and S Narasimhan ldquoSmart base-isolated bench-mark building Part II Phase I sample controllers for linearisolation systemsrdquo Structural Control and Health Monitoringvol 13 no 2-3 pp 605ndash625 2006

Submit your manuscripts athttpwwwhindawicom

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

MathematicsJournal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Mathematical Problems in Engineering

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Differential EquationsInternational Journal of

Volume 2014

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Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

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CombinatoricsHindawi Publishing Corporationhttpwwwhindawicom Volume 2014

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Function Spaces

Abstract and Applied AnalysisHindawi Publishing Corporationhttpwwwhindawicom Volume 2014

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Algebra

Discrete Dynamics in Nature and Society

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

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Decision SciencesAdvances in

Discrete MathematicsJournal of

Hindawi Publishing Corporationhttpwwwhindawicom

Volume 2014 Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Stochastic AnalysisInternational Journal of

6 Mathematical Problems in Engineering

the time history of the generated artificial earthquakes for softsoil is distinct with the other Particularly the peak velocityreaches 09ms which is significantly greater than the other

3 Model of Base-Isolated Structure andPiezoelectric Friction Damper

31 Equation of Motion for Base-Isolated Structure Consideran n-degree of freedom base-isolated structure with a piezo-electric friction damper at the isolation floor the dynamicequation of the base-isolated system is given by

MX (119905) + CX (119905) + KX (119905) = B119904U (119905) + E

119904119892(119905) (2)

where M C and K represent 119899 times 119899 mass damping andstiffness matrices respectively X(119905) X(119905) and X(119905) are theacceleration velocity and displacement vectors respectivelyU(119905) is the control force generated by the piezoelectric frictiondamper and

119892(119905) is the earthquake acceleration

Rewriting (2) in state-space form gives

Z (119905) = AZ (119905) + BU (119905) + E119892(119905) (3)

where

Z (119905) = [X (119905)X (119905)

]

E = [0119899times1

Mminus1E119904

]

B = [0119899times1

Mminus1B119904

]

A = [0119899times119899

I119899times119899

minusMminus1K minusMminus1C]

(4)

32 Model of Piezoelectric Friction Damper Piezoelectricfriction damper is a novel semiactive control device whichutilizes piezoelectric stacks to regulate the damping forceto provide a satisfying level of friction force Recently theauthors also proposed a piezoelectric friction damper andinvestigated their performances theoretically and experimen-tally [17]

During the movement of the base-isolated structure afriction damper has two possible motion states sticking andslipping phases [18 19] The friction force of the piezoelectricfriction damper is given as [20]

119873(119905) = 119873pre + 119862pz119881 (119905)

119891 (119905) = minus120583119873 (119905) sgn () = 0

minus120583119873 (119905) le 119891 (119905) le 120583119873 (119905) = 0

(5)

where 119873(119905) is the total contact force 119873pre represents thepreload of the piezoelectric friction damper 119862pz is thepiezoelectric coefficient of the piezoelectric actuator 119881(119905)is the input voltage of piezoelectric stack actuator 120583 is the

Table 3 Parameters of piezoelectric friction damper

Parameters Values120583 04119862pz 1125NV119881max 1000V

friction coefficient of the damper sgn(sdot) represents the signfunction related to the slip rate of the damper and 119891(119905)denotes damping force of piezoelectric friction damper

However the static state of the piezoelectric frictiondamper is complex to be estimated Shook et al [21] proposedan approximate calculation formula for the sticking frictionforce as given in the following

119891119904= minus120583119873 (119905) sgn ()

when 119891119904=1003816100381610038161003816119891119894 + 119891119903

1003816100381610038161003816 1003816100381610038161003816119891 (119905)

1003816100381610038161003816 ge 119891119904

119891119894= 119898119905119892= (119898

119887+

119899

sum

119894=1

119898119894) 119892

119891119903= 119896119887119909119887

(6)

where 119891119894is the inertial force applied on the mass 119891

119903is the

restoring force provided by the isolation bearing 119898119894is the

mass of the superstructure 119898119887and 119896

119887are the mass and

stiffness of base isolator and 119909119887is the displacement of base

isolatorThe parameters of piezoelectric friction damper are listed

in Table 3 And the preload of the piezoelectric frictiondamper can be optimized by genetic algorithm

4 GA-Based Hierarchic Fuzzy ControlAlgorithm

41 Framework of the Developed Fuzzy Logic Controller Thecontroller adopts a hierarchic fuzzy control algorithm inwhich a supervisory fuzzy controller governs a sublevelfuzzy controller by altering its input normalization factorsaccording to the current level of groundmotionThe sublevelfuzzy logic controller is designed to determine the commandvoltage of piezoelectric friction damper according to thevelocity and displacement of base isolation Piezoelectricfriction damper regulates the damping force according tothe input voltage Genetic algorithm is employed to optimizesupervisory fuzzy controller and preload of piezoelectricfriction damper according to an objective function and thegenerated artificial earthquakes for different ground sitesTheblock diagram of the system for the developed controller isshown in Figure 7

42 Sublevel Fuzzy Controller The sublevel fuzzy controlleris established in order to determine the command voltage ofthe piezoelectric friction damper The isolation displacementand velocity are selected as two input variables and commandvoltage is employed as a single output variable as shown inFigure 8The definitions of themembership function of input

Mathematical Problems in Engineering 7

Ground motion

Damping force

Semiactiveisolated

structure

Piezoelectricfriction damper

Ground velocity

Optimize

Voltage

Structural response

Isolation velocity and displacement

Sublevel fuzzycontroller

Supervisoryfuzzy controller

Optimize

Genetic algorithm

Nd

N

Figure 7 Block diagram of the base-isolated system for the fuzzy controller

minus10 minus05 00 05 100

1PL

PMPSZENSNM

Deg

ree o

f mem

bers

hip

Normalized displacement

NL

00 05 100

1PL

PMPSZENSNM

Deg

ree o

f mem

bers

hip

Normalized velocity

NL

0 200 400 600 800 10000

1VL

LMS

Deg

ree o

f mem

bers

hip

Voltage (V)

ZE

minus10 minus05

Figure 8 Input and output membership functions of sublevel fuzzy control

variables are as follows NL negative large NM negativemedium NS negative small ZE zero PS positive small PMpositive medium and PL positive large The definition ofthe membership function of output variable is as follows ZEzero S small M medium L large and VL very large Themembership functions are employed Gaussian type for inputand output variables The fuzzy control rules are defined inTable 4

In the establishment of fuzzy control rules it followsthe following principles if the isolation displacement andvelocity are in opposite sign then the output voltage becomessmall in order to ensure output small damping force inthe piezoelectric friction damper Contrarily if the isolationdisplacement and velocity have the same sign the outputvoltage becomes large Certainly when the displacement andvelocity are almost zero or small the command voltage is

8 Mathematical Problems in Engineering

Table 4 Fuzzy control rules adopted for sublevel fuzzy control

Velocity ofisolated floor

Displacement of isolated floorNL NM NS ZE PS PM PL

NL VL VL L L M S ZENM VL L L M S ZE SNS L L M S ZE S MZE L M S ZE S M LPS M S ZE S M L LPM S ZE S M L L VLPL ZE S M L L VL VL

minus1minus05

005

1

minus1minus05

005

1

500

1000

VelocityDisplacement

Volta

ge (V

)

Figure 9 Fuzzy control surface for sublevel fuzzy controller

about zero this means that piezoelectric friction damper actsas a passive friction damper The defuzzification of fuzzycontrol adopts the method of centroid to get a crisp outputvalue The control surface and color-filled contour line ofsublevel fuzzy control are depicted in Figure 9

43 Supervisory Fuzzy Logic Controller In the fuzzy logiccontrol normalization factors need to satisfy a certain objec-tive The oversize normalization factors can enlarge the basedisplacement effectively Contrarily too small normalizationfactors can result in large control force that amplifies theaccelerations of base-isolated structure Thus a supervisoryfuzzy logic control is proposed to adjust its normalizationfactors in real-time As discussed earlier near-fault earth-quakes usually have long duration pulses with peak velocitiesThus the supervisory fuzzy control employs ground velocityas single input variable to identify the characteristics ofthe ground motion The normalization factors of sublevelfuzzy control are selected as two output variables HereGaussian membership functions are used for input andoutput variables as shown in

120583gauss = exp[minus(119909 minus 119888)2

21205902] (7)

where 119888 and 120590 are the constant values that define the shape ofthe Gauss functions respectively

The rules of the supervisory fuzzy controller are definedby the following form

Rule119894 IF 119883 is 119860119894 then 1198841is 1198621198941 1198842is 1198621198942

119894 = 1 2 119872

(8)

where119872 is the number of fuzzy control rules 119883 is the inputvariable 119884

1and 119884

2are the output variables 119860119894 119862119894

1 and 119862119894

2

are the linguistic values characterized by input and outputmembership functions respectively One fuzzy control ruleis described by three Gaussian membership functions andeach membership function can be defined by two parameters(119888 and 120590) Therefore a total of five fuzzy control rules canbe optimized by encoding these two parameters into thegene using genetic algorithm Consequently a total of 30parameters are encoded into the chromosome to define theinference system of supervisory fuzzy controller as shown inFigure 10

Similar to normalization factors the preload of thepiezoelectric friction dampers has a great influence on thedamping effect Thus it is essential to establish an effectivesupervisory fuzzy logic controller and a suitable preloadof piezoelectric friction damper Generally for the seismicprotection of a base-isolated structure there is a trade-off between the isolation displacement and superstructureacceleration The main control objective is to depress theisolation displacementwithout excessively increasing acceler-ation response of the superstructure In this section a geneticalgorithm is employed to seek out an optimal solution forthe control of the base-isolated structure The flow chart ofgenetic algorithm is shown in Figure 11

Genetic algorithm is a computational model for thesimulation of Darwin natural genetic selection and biologicalevolution Different from the traditional search algorithmgenetic algorithm begins to search a group of optimal solu-tions from an initial random population by mutation andrecombination Each individual which consists of a set ofbinary strings is a solution to the objective problem Afterinitialization genetic algorithm uses a sort method to rankindividuals It compares each solution with other solutionsin the population to find whether it is dominated Duringthe process of creating a new generation it selects a suitableindividual according to the size of the fitness value Afterseveral generations the individual value gradually convergesto the best chromosome which is the optimal solution

The objective fitness function employed in this study isshown as follows

119869 = 06 times119910119887max

119910119887max

+ 04 timesradicsum119899

119894=1(119886119894max119886119894max)

2

119899 (9)

where 119910119887max and 119910119887max denote the peak base displacements

for the fuzzy control and uncontrolled cases respectively119886119894max and 119886119894max represent the peak superstructure accelera-tion for the fuzzy control and uncontrolled case respectively

The objective of genetic algorithm is tomake the objectivefitness function reach its minimum value by selecting oneset of parameters of supervisory fuzzy control and preload

Mathematical Problems in Engineering 9

0

1

X

0

1

Deg

ree o

f mem

bers

hip

Deg

ree o

f mem

bers

hip

0

1

Deg

ree o

f mem

bers

hip

1205901

1205901 1205902 1205903

Rule 1 (1 6) Rule 1 (7 12) Rule 5 (24 30)middot middot middot

c1

c1 c2 c3

1205902

Y1

1205903

Y2c2 c3

Figure 10 Encoding structure for genetic algorithm

of piezoelectric friction damper The initial population sizegenetic algebra and crossover probability are set to 20 50and 08 respectively Through inputting the artificial earth-quakes which are characterized by near-fault earthquakesfor different ground sites the supervisory fuzzy control andpreload of piezoelectric friction dampers can be optimizedThe fuzzy control surfaces of optimized supervisory fuzzycontrol are shown in Figure 12

5 Linear Quadratic Gaussian Controller

LQG (Linear Quadratic Gaussian) method is based onKalman filter technique which has become a widely usedcontrol algorithm For comparison purpose LQG is adoptedto regulate the contact normal force of piezoelectric frictiondamper in the study The optimal controller takes groundacceleration as white noise and considers the velocity anddisplacement of base isolation as feedback signals Thecontrol performance index is defined as follows [22]

119869 = lim120591rarr+infin

1

120591

sdot 119864 int

120591

0

[Z (119905)119879QZ (119905) + U (119905)119879RU (119905)] 119889 (119905) (10)

where Q2119899times2119899

and R1times1

are semi-positive definite matrix andpositive definite matrix respectivelyThe control force can beobtained as follows

U (119905) = minusGZ (119905) (11)

G = Rminus1B119879P (12)

where P can be computed by the solution of the Riccatiequation as follows

minusPA minus A119879P + PBRminus1B119879P minusQ = 0 (13)

The control force obtained from the above equation isactive control force which could not be always achieved bypiezoelectric friction damper It is realized that the directionof active control force is opposite to the slipping direction ofpiezoelectric friction damper Therefore the desired controlforce119906

119889(119905) can be achieved according to the following criteria

119906119889(119905)

=

119891max sgn (119887) (119906active

119887lt 0

10038161003816100381610038161003816119906active10038161003816100381610038161003816 gt 119891max)

10038161003816100381610038161003816119906active10038161003816100381610038161003816 sgn (119887) (119906

active119887lt 0

10038161003816100381610038161003816119906active10038161003816100381610038161003816 le 119891max)

119891min sgn (119887) (119906active

119887ge 0)

(14)

10 Mathematical Problems in Engineering

Table 5 Parameters of base-isolated structure

Floor masses(kg)

Stiffness values(kNm)

Dampingcoefficients(kN sm)

Isolated floor 6800 232 745First floor 5897 33732 67Second floor 5897 29093 58Third floor 5897 28621 57Fourth floor 5897 24954 50Fifth floor 5897 19059 38

No

Yes

Encode

Generate initial random population

Calculate the value of fitness and rank

Copy crossover and mutation

Decode

Optimal solution

Whether or not to meet thecondition of convergence

Figure 11 Flow chart of genetic algorithm

where 119906active is the control force obtained from LQG con-troller

119887is the velocity of base isolator119891max and119891min are the

maximum and minimum friction forces of the piezoelectricfriction damper respectively

6 Numerical Simulations

61 Model of the Base-Isolated Structure A five-story base-isolated building which is proposed by He et al is employedto evaluate the performance of developed fuzzy controllers[18] The fundamental period of the five-story building is03 s For the given isolation parameters the fundamentalperiod of the base-isolated building becomes 25 sThereforean isolation ratio 120575 equal to 83 (=2503) is obtainedThe model of the base-isolated structure with piezoelectricfriction damper is shown in Figure 13 The parameters of thebase-isolated structure are shown in Table 5

62 Performance Evaluation Index In order to evaluate theperformance of base-isolated structure for different controlalgorithms a total of nine performance indexes are employedin this study [23] as shown in Table 6

The performance indexes J1through J

5denote the struc-

ture responses for the controlled building normalized byuncontrolled structure respectively The performance indexJ6evaluates the peak control force normalized by the peak

base shear for controlled structure The performance indexesJ7and J8represent RMS (Root Mean Square) base displace-

ments and RMS floor accelerations respectively J9computes

the energy dissipated by friction dampers normalized by theearthquake input energy to the controlled structure

63 Simulation Results and Analysis A total of nine seis-mic excitations that contain six real ground motions andthree artificial earthquakes are selected to evaluate the per-formance of the optimized fuzzy logic controller In thisstudy the time histories of strong earthquake which rangefrom 20 s to 70 s are selected for numerical simulation andanalysis

The numerical results for various earthquakes are listedin Table 7 In the table the Genetic Algorithm HierarchicFuzzy Logic Control is named as GHFLC Moreover forcomparison purpose the results for an optimal controller andpassive operation of friction damper are also listed in thetable Numbers in bold font indicate the best results amongall control cases

Base displacement is an important index to evaluatethe effectiveness for different controllers For a base-isolatedstructure the reduction of base displacement is a primarypurpose to prevent permanent damage for isolation bearingsor adjacent buildings Although passive operation of frictiondampers can successfully reduce the performance indexassociated with the peak and RMS base displacements (J

3and

J7) it causes significant amplification in peak and RMS floor

accelerations (J5and J

8) for most cases due to the passive

control For example as compared to the uncontrolledstructure for TCU052 TCU053 and TCU054 earthquakespassive control leads to 6 45 and 42 amplification inpeak floor acceleration respectively However the proposedfuzzy controller can successfully improve the base-isolatedstructure acceleration at the cost of slight deterioration in theperformance indices J

3and J7on comparison with passive

control For example for TCU052 TCU053 and TCU054earthquakes GHFLC results in 15 13 and 16 decrease inpeak floor accelerations respectively As compared to passivecontrol there are 9 3 and 7 increase in peak basedisplacements

The time histories of friction force and force-displacement curves of friction dampers for differentcontrollers subjected to TCU052 earthquake are shown inFigure 14 From the figures it can be seen that the passivecontrol outputs lager damper force than GHFLC Becausethe supervisory fuzzy control can alter input normalizationfactors of sublevel FLC according to the current level ofground motion there are some serrations presented at theedge of the hysteretic curve of piezoelectric friction damper

The comparison of the performance indexes J3 J7 J5and

J8under different control cases is shown in Figures 15 and

16 respectively From these figures it can be seen that thefuzzy controller is more effective than passive and optimal

Mathematical Problems in Engineering 11O

utpu

t

009

055

026

000033

000094000

Input ground velocity (ms)

Nd

N

(a) Hard soilO

utpu

t

Input ground velocity (ms)

071

042

000

008000

037

103000

Nd

N

(b) Medium soil

Out

put

Input ground velocity (ms)

107

053

000045

011000

117000

Nd

N

(c) Soft soil

Figure 12 Control surface for optimized supervisory fuzzy control

PFD

Fixed reference

LRB

Figure 13 Model of the base-isolated structure

12 Mathematical Problems in Engineering

Table 6 Performance index

Peak base shear Peak interstory drift RMS base displacement

1198691=max119905

10038171003817100381710038171198810 (119905)1003817100381710038171003817

max119905

100381710038171003817100381710038171198810(119905)10038171003817100381710038171003817

1198694=

max119905119891

10038171003817100381710038171003817119889119891(119905)10038171003817100381710038171003817

max119905119891

10038171003817100381710038171003817119889119891(119905)10038171003817100381710038171003817

1198697=

max119894

1003817100381710038171003817120590119889 (119905)1003817100381710038171003817

max119905

1003817100381710038171003817119889 (119905)1003817100381710038171003817

Peak structural shear Peak floor acceleration RMS floor acceleration

1198692=max119905

10038171003817100381710038171198811 (119905)1003817100381710038171003817

max119905

100381710038171003817100381710038171198811(119905)10038171003817100381710038171003817

1198695=

max119905119891

10038171003817100381710038171003817119886119891(119905)10038171003817100381710038171003817

max119905119891

10038171003817100381710038171003817119886119891(119905)10038171003817100381710038171003817

1198698=max119891

1003817100381710038171003817120590119886 (119905)1003817100381710038171003817

max119891

1003817100381710038171003817119886 (119905)1003817100381710038171003817

Peak base displacement Peak control force Energy dissipated by PFD

1198693=max119905

1003817100381710038171003817119909119887 (119905)1003817100381710038171003817

max119905

1003817100381710038171003817119909119887 (119905)1003817100381710038171003817

1198696=max119905

1003817100381710038171003817119891119889 (119905)1003817100381710038171003817

max119905

10038171003817100381710038171198810 (119905)1003817100381710038171003817

1198699=

int119879

0

119891119889(119905) 119887(119905) 119889119905

int119879

0

1198810(119905) 119892(119905) 119889119905

Table 7 Results of numerical simulation

Earthquake Control case 1198691

1198692

1198693

1198694

1198695

1198696

1198697

1198698

1198699

TCU102(hard site)

Passive 081 082 068 085 094 048 057 082 078Optimal 092 095 075 099 087 043 068 081 069GHFLC 087 091 071 093 082 041 061 078 073

TCU052(hard site)

Passive 079 079 046 082 106 036 038 089 087Optimal 087 087 057 087 098 029 049 085 079GHFLC 083 082 055 082 091 033 044 079 084

Artificialearthquake(hard site)

Passive 072 074 054 076 092 054 049 090 084Optimal 084 086 069 083 089 047 057 086 073GHFLC 076 077 061 079 083 042 052 081 076

TCU053(medium site)

Passive 061 065 039 071 145 032 037 116 089Optimal 069 072 046 076 136 031 045 117 078GHFLC 062 062 042 065 132 026 044 109 072

TCU054(medium site)

Passive 071 073 043 073 142 084 038 121 088Optimal 081 087 045 085 132 079 052 125 086GHFLC 075 071 040 074 126 082 045 113 076

Artificialearthquake(medium site)

Passive 054 057 038 064 123 067 036 117 091Optimal 067 066 047 067 119 078 048 113 079GHFLC 058 061 040 062 113 072 041 109 085

TCU110(soft soil site)

Passive 077 078 047 077 103 050 045 089 095Optimal 083 082 052 085 107 046 052 099 087GHFLC 086 086 056 086 104 042 049 093 090

CHY101(soft soil site)

Passive 069 071 058 075 086 066 054 092 084Optimal 075 073 062 074 087 064 055 088 079GHFLC 063 067 054 067 079 065 051 087 083

Artificialearthquake(soft site)

Passive 057 064 061 068 097 061 058 098 088Optimal 071 070 074 075 094 058 071 093 083GHFLC 065 062 067 069 085 055 063 086 076

controller in simultaneously depressing the superstructureacceleration and base displacement For example the appli-cation of developed fuzzy controller leads to an average of112 decrease in peak floor acceleration and an average ofonly 36 increase in peak base displacement as compared topassive control Particularly optimal controller produces anaverage of only 41 reduction in peak floor acceleration and

leads to 79 increase in peak base displacement as comparedto passive control Therefore the improved fuzzy controlmethod shows better performance than passive and optimalcontrol

In order to further evaluate the performance of differentcontrollers the energy time histories for different controllersare compared with each other For a base-isolated structure

Mathematical Problems in Engineering 13

20 30 40 50 60 70minus20

minus10

00

10

20Fr

ictio

n fo

rce (

kN)

Time (s)minus03 minus02 minus01 00 01 02 03

minus20

minus10

00

10

20

Fric

tion

forc

e (kN

)

Displacement (m)

(a) Passive control

20 30 40 50 60 70minus20

minus10

00

10

20

Fric

tion

forc

e (kN

)

Time (s)minus03 minus02 minus01 00 01 02 03

minus20

minus10

00

10

20

Fric

tion

forc

e (kN

)

Displacement (m)

(b) GHFLC method

Figure 14 Time histories of friction force and force-displacement diagram against TCU052 earthquake

1 2 3 4 5 6 7 8 903

04

05

06

07

08

Excitation case

Passive OptimalGHFLC

1 2 3 4 5 6 7 8 903

04

05

06

07

Excitation casePassive

GHFLC Optimal

J 3 J 5

Figure 15 Comparisons on the performance indexes J3and J7for different control cases

14 Mathematical Problems in Engineering

1 2 3 4 5 6 7 8 907

08

09

10

11

12

13

14

15

Excitation casePassive

GHFLC Optimal

1 2 3 4 5 6 7 8 907

08

09

10

11

12

13

Excitation case

Passive

GHFLC Optimal

J 8J 5

Figure 16 Comparison of the performance indexes J5and J8for different control cases

with piezoelectric friction dampers installed on the isolationthe energy equations are defined as follows

119864119870+ 119864120585+ 119864119878+ 119864119867= 119864119868

119864119870=1

2119879

119905119872119905

119864120585= int

119905

0

119879

119888 119889119905

119864119878= int

119905

0

119909119879

119870119889119909

119864119867= minusint

119905

0

119906119879

119864119879

119904119889119909

119864119868= minusint

119905

0

gMI 119889119909

(15)

where 119864119870 119864120585 119864119878 119864119867 and 119864

119868denote the absolute kinetic

energy damping energy elastic strain energy energy dis-sipated by piezoelectric friction dampers and total inputenergy respectively The energy time histories for differentcontrollers against TCU052Chi-Chi earthquake are shown inFigure 17 It can be seen from the figures that the piezoelectricfriction dampers dissipate most of the input energy fordifferent control cases subjected to TCU052 earthquake

In order to compare different effects under near-faultground motions recorded for different sites the average ofinput energy and structure responses subjected to near-faultearthquakes are given in Table 8

As shown in Table 8 the near-fault earthquakes forsoft sites are more destructive than hard sites For instancecompared to hard sites the input energy and the base dis-placement of RMS of the base-isolated structure for soft soil

increase by 143 and 256 respectively However GHFLCpossesses favorable performance under different ground sitesand the damping effect has no distinctly direct relationshipwith site category

As discussed in Section 61 the isolation ratio of thesimulation model equals 83 In order to evaluate the effectsof isolation ratio on the damping performance of GHFLC thestiffness value of isolation is adjusted to 1045 and 452 kNmrespectively Then the numerical results for different valuesof isolation ratio (120575 = 4 6) are obtained The performanceindexes J

3and J5for different isolation ratios are shown in

Figures 18 and 19 respectivelyFor base-isolated structure isolation ratio has a signifi-

cant influence on the isolation effect A larger isolation ratiowhich means a minor stiffness value of isolation usuallyleads to conspicuous enlargement of base displacement anddecrease of superstructural responses due to the increaseof fundamental vibration period and vice versa Howeveras shown in Figures 18 and 19 the shock absorption rateof GHFLC has little change when isolation ratio variesdifferently and the proposed fuzzy control shows favorableeffectiveness in the diverse isolation ratios of base-isolatedstructures

7 Conclusions

In this study an optimized fuzzy logic control which isdesigned for Chi-Chi near-fault earthquakes under differentground sites is proposed An elastic design spectrum isproposed to generate near-fault earthquakes for differentground sitesThe characteristic of the design spectrum is thatit has larger periods and peak acceleration than conventionalspectrum Genetic algorithm is employed to optimize thesupervisory fuzzy controller and preload of piezoelectric

Mathematical Problems in Engineering 15

Table 8 Average ofinput energy and structure responses subjected to near-fault earthquakes

Site classification Input energy (kNsdotm) Base shear (kN) Base displacement ofRMS (m)

Structure accelerationof RMS (g)

Hard soil 24375 475 0047 0432Medium soil 26746 498 0054 0476Soft soil 27857 568 0059 0531

20 30 40 50 60 7000

05

10

15

20

25

Input energyEnergy dissipated by dampers

Time (s)

Ener

gy (k

Nmiddotm

)

times104

(a) Passive control

20 30 40 50 60 7000

05

10

15

20

25

30

Time (s)

Input energyEnergy dissipated by dampers

Ener

gy (k

Nmiddotm

)

times104

(b) Optimal control

20 30 40 50 60 7000

05

10

15

20

25

30

Input energyEnergy dissipated by dampers

Time (s)

Ener

gy (k

Nmiddotm

)

times104

(c) GHFLC method

Figure 17 Energy time histories subjected to Chi-Chi TCU052 earthquake

friction dampers according to three artificial earthquakesthat are characterized by Chi-Chi earthquakes Passive andoptimal controllers are also compared with the performanceof the developed fuzzy controller The simulation resultsreveal that the developed semiactive fuzzy controller hasbetter performance than traditional passive and optimal con-troller in simultaneously reducing the base displacement and

floor acceleration under near-fault earthquakes for differentground sites

Conflict of Interests

The authors declare no conflict of interests regarding thepublication of this paper

16 Mathematical Problems in Engineering

1 2 3 4 5 6 7 8 903

04

05

06

07

08

Excitation casePassive

GHFLC Optimal

1 2 3 4 5 6 7 8 907

08

09

10

11

12

13

14

15

Excitation case

Passive

GHFLC Optimal

J 3 J 5Figure 18 Comparisons on the performance indexes J

3and J5for different control cases (120575 = 4)

1 2 3 4 5 6 7 8 903

04

05

06

07

08

Excitation casePassive

GHFLC Optimal

1 2 3 4 5 6 7 8 907

08

09

10

11

12

13

14

15

Excitation casePassive

GHFLC Optimal

J 3 J 5

Figure 19 Comparisons on the performance indexes J3and J5for different control cases (120575 = 6)

Acknowledgments

This research was supported by National Natural ScienceFoundation of China under Grant no 51308487 no 41402261and no 51408526 Hebei Provincial Natural Science Founda-tion ofChina underGrant no E2014203055 and the ExcellentYouth Foundation of Hebei Educational Committee underGrant no YQ2013015 The support for this research is greatlyappreciated

References

[1] C Alhan and H Gavin ldquoA parametric study of linear and non-linear passively damped seismic isolation systems for buildingsrdquoEngineering Structures vol 26 no 4 pp 485ndash497 2004

[2] R S Jangid and J M Kelly ldquoBase isolation for near-faultmotionsrdquoEarthquake Engineering and Structural Dynamics vol30 no 5 pp 691ndash707 2001

[3] J Shen M-H Tsai K-C Chang and G C Lee ldquoPerformanceof a seismically isolated bridge under near-fault earthquake

Mathematical Problems in Engineering 17

ground motionsrdquo Journal of Structural Engineering vol 130 no6 pp 861ndash868 2004

[4] F Mazza A Vulcano and M Mazza ldquoNonlinear dynamicresponse of RC buildings with different base Isolation systemssubjected to horizontal and vertical components of near-faultground motionsrdquo Open Construction and Building TechnologyJournal vol 6 pp 373ndash383 2012

[5] F Mazza and A Vulcano ldquoEffects of near-fault ground motionson the nonlinear dynamic response of base-isolated rc framedbuildingsrdquo Earthquake Engineering and Structural Dynamicsvol 41 no 2 pp 211ndash232 2012

[6] O E Ozbulut and S Hurlebaus ldquoFuzzy control of piezoelectricfriction dampers for seismic protection of smart base isolatedbuildingsrdquo Bulletin of Earthquake Engineering vol 8 no 6 pp1435ndash1455 2010

[7] O E Ozbulut M Bitaraf and S Hurlebaus ldquoAdaptive controlof base-isolated structures against near-field earthquakes usingvariable friction dampersrdquo Engineering Structures vol 33 no12 pp 3143ndash3154 2011

[8] J M Kelly ldquoThe role of damping in seismic isolationrdquo Earth-quake Engineering and Structural Dynamics vol 28 no 1 pp3ndash20 1999

[9] F Mazza and A Vulcano ldquoNonlinear response of RC framedbuildings with isolation and supplemental damping at the basesubjected to near-fault earthquakesrdquo Journal of EarthquakeEngineering vol 13 no 5 pp 690ndash715 2009

[10] M Bitaraf and S Hurlebaus ldquoSemi-active adaptive control ofseismically excited 20-story nonlinear buildingrdquo EngineeringStructures vol 56 no 11 pp 2107ndash2118 2013

[11] D Das T K Datta and A Madan ldquoSemiactive fuzzy controlof the seismic response of building frames with MR dampersrdquoEarthquake Engineering and Structural Dynamics vol 41 no 1pp 99ndash118 2012

[12] A-P Wang and C-D Lee ldquoFuzzy sliding mode control for abuilding structure based on genetic algorithmsrdquo EarthquakeEngineering and Structural Dynamics vol 31 no 4 pp 881ndash8952002

[13] D G Reigles and M D Symans ldquoSupervisory fuzzy controlof a base-isolated benchmark building utilizing a neuro-fuzzymodel of controllable fluid viscous dampersrdquo Structural Controland Health Monitoring vol 13 no 2-3 pp 724ndash747 2006

[14] H-S Kim and P N Roschke ldquoGA-fuzzy control of smartbase isolated benchmark building using supervisory controltechniquerdquo Advances in Engineering Software vol 38 no 7 pp453ndash465 2007

[15] D Yang and Y Zhao ldquoEffects of rupture forward directivity andfling step of near-fault groundmotions on seismic performanceof base-isolated building structurerdquo Acta Seismologica Sinicavol 32 no 5 pp 579ndash587 2010

[16] Y E-A Mohamedzein J A Abdalla and A Abdelwahab ldquoSiteresponse and earthquake design spectra for central KhartoumSudanrdquoBulletin of Earthquake Engineering vol 4 no 3 pp 277ndash293 2006

[17] D Zhao and H Li ldquoShaking table tests and analyses of semi-active fuzzy control for structural seismic reduction with apiezoelectric variable-friction damperrdquo Smart Materials andStructures vol 19 no 10 Article ID 105031 2010

[18] W L He A K Agrawal and J N Yang ldquoNovel semiactivefriction controller for linear structures against earthquakesrdquoJournal of Structural Engineering vol 129 no 7 pp 941ndash9502003

[19] J N Yang and A K Agrawal ldquoSemi-active hybrid controlsystems for nonlinear buildings against near-field earthquakesrdquoEngineering Structures vol 24 no 3 pp 271ndash280 2002

[20] O E Ozbulut and S Hurlebaus ldquoOptimal design of supere-lastic-friction base isolators for seismic protection of highwaybridges against near-field earthquakesrdquo Earthquake Engineeringand Structural Dynamics vol 40 no 3 pp 273ndash291 2011

[21] D A Shook P N Roschke and O E Ozbulut ldquoSuperelasticsemi-active damping of a base-isolated structurerdquo StructuralControl and HealthMonitoring vol 15 no 5 pp 746ndash768 2008

[22] K D PhamG JinM K Sain B F Spencer Jr and S R LibertyldquoGeneralized linear quadratic Gaussian techniques for the windbenchmark problemrdquo Journal of Engineering Mechanics vol130 no 4 pp 466ndash470 2004

[23] S Nagarajaiah and S Narasimhan ldquoSmart base-isolated bench-mark building Part II Phase I sample controllers for linearisolation systemsrdquo Structural Control and Health Monitoringvol 13 no 2-3 pp 605ndash625 2006

Submit your manuscripts athttpwwwhindawicom

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

MathematicsJournal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Mathematical Problems in Engineering

Hindawi Publishing Corporationhttpwwwhindawicom

Differential EquationsInternational Journal of

Volume 2014

Applied MathematicsJournal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Probability and StatisticsHindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Journal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Mathematical PhysicsAdvances in

Complex AnalysisJournal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

OptimizationJournal of

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CombinatoricsHindawi Publishing Corporationhttpwwwhindawicom Volume 2014

International Journal of

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Operations ResearchAdvances in

Journal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Function Spaces

Abstract and Applied AnalysisHindawi Publishing Corporationhttpwwwhindawicom Volume 2014

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Algebra

Discrete Dynamics in Nature and Society

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

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Decision SciencesAdvances in

Discrete MathematicsJournal of

Hindawi Publishing Corporationhttpwwwhindawicom

Volume 2014 Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Stochastic AnalysisInternational Journal of

Mathematical Problems in Engineering 7

Ground motion

Damping force

Semiactiveisolated

structure

Piezoelectricfriction damper

Ground velocity

Optimize

Voltage

Structural response

Isolation velocity and displacement

Sublevel fuzzycontroller

Supervisoryfuzzy controller

Optimize

Genetic algorithm

Nd

N

Figure 7 Block diagram of the base-isolated system for the fuzzy controller

minus10 minus05 00 05 100

1PL

PMPSZENSNM

Deg

ree o

f mem

bers

hip

Normalized displacement

NL

00 05 100

1PL

PMPSZENSNM

Deg

ree o

f mem

bers

hip

Normalized velocity

NL

0 200 400 600 800 10000

1VL

LMS

Deg

ree o

f mem

bers

hip

Voltage (V)

ZE

minus10 minus05

Figure 8 Input and output membership functions of sublevel fuzzy control

variables are as follows NL negative large NM negativemedium NS negative small ZE zero PS positive small PMpositive medium and PL positive large The definition ofthe membership function of output variable is as follows ZEzero S small M medium L large and VL very large Themembership functions are employed Gaussian type for inputand output variables The fuzzy control rules are defined inTable 4

In the establishment of fuzzy control rules it followsthe following principles if the isolation displacement andvelocity are in opposite sign then the output voltage becomessmall in order to ensure output small damping force inthe piezoelectric friction damper Contrarily if the isolationdisplacement and velocity have the same sign the outputvoltage becomes large Certainly when the displacement andvelocity are almost zero or small the command voltage is

8 Mathematical Problems in Engineering

Table 4 Fuzzy control rules adopted for sublevel fuzzy control

Velocity ofisolated floor

Displacement of isolated floorNL NM NS ZE PS PM PL

NL VL VL L L M S ZENM VL L L M S ZE SNS L L M S ZE S MZE L M S ZE S M LPS M S ZE S M L LPM S ZE S M L L VLPL ZE S M L L VL VL

minus1minus05

005

1

minus1minus05

005

1

500

1000

VelocityDisplacement

Volta

ge (V

)

Figure 9 Fuzzy control surface for sublevel fuzzy controller

about zero this means that piezoelectric friction damper actsas a passive friction damper The defuzzification of fuzzycontrol adopts the method of centroid to get a crisp outputvalue The control surface and color-filled contour line ofsublevel fuzzy control are depicted in Figure 9

43 Supervisory Fuzzy Logic Controller In the fuzzy logiccontrol normalization factors need to satisfy a certain objec-tive The oversize normalization factors can enlarge the basedisplacement effectively Contrarily too small normalizationfactors can result in large control force that amplifies theaccelerations of base-isolated structure Thus a supervisoryfuzzy logic control is proposed to adjust its normalizationfactors in real-time As discussed earlier near-fault earth-quakes usually have long duration pulses with peak velocitiesThus the supervisory fuzzy control employs ground velocityas single input variable to identify the characteristics ofthe ground motion The normalization factors of sublevelfuzzy control are selected as two output variables HereGaussian membership functions are used for input andoutput variables as shown in

120583gauss = exp[minus(119909 minus 119888)2

21205902] (7)

where 119888 and 120590 are the constant values that define the shape ofthe Gauss functions respectively

The rules of the supervisory fuzzy controller are definedby the following form

Rule119894 IF 119883 is 119860119894 then 1198841is 1198621198941 1198842is 1198621198942

119894 = 1 2 119872

(8)

where119872 is the number of fuzzy control rules 119883 is the inputvariable 119884

1and 119884

2are the output variables 119860119894 119862119894

1 and 119862119894

2

are the linguistic values characterized by input and outputmembership functions respectively One fuzzy control ruleis described by three Gaussian membership functions andeach membership function can be defined by two parameters(119888 and 120590) Therefore a total of five fuzzy control rules canbe optimized by encoding these two parameters into thegene using genetic algorithm Consequently a total of 30parameters are encoded into the chromosome to define theinference system of supervisory fuzzy controller as shown inFigure 10

Similar to normalization factors the preload of thepiezoelectric friction dampers has a great influence on thedamping effect Thus it is essential to establish an effectivesupervisory fuzzy logic controller and a suitable preloadof piezoelectric friction damper Generally for the seismicprotection of a base-isolated structure there is a trade-off between the isolation displacement and superstructureacceleration The main control objective is to depress theisolation displacementwithout excessively increasing acceler-ation response of the superstructure In this section a geneticalgorithm is employed to seek out an optimal solution forthe control of the base-isolated structure The flow chart ofgenetic algorithm is shown in Figure 11

Genetic algorithm is a computational model for thesimulation of Darwin natural genetic selection and biologicalevolution Different from the traditional search algorithmgenetic algorithm begins to search a group of optimal solu-tions from an initial random population by mutation andrecombination Each individual which consists of a set ofbinary strings is a solution to the objective problem Afterinitialization genetic algorithm uses a sort method to rankindividuals It compares each solution with other solutionsin the population to find whether it is dominated Duringthe process of creating a new generation it selects a suitableindividual according to the size of the fitness value Afterseveral generations the individual value gradually convergesto the best chromosome which is the optimal solution

The objective fitness function employed in this study isshown as follows

119869 = 06 times119910119887max

119910119887max

+ 04 timesradicsum119899

119894=1(119886119894max119886119894max)

2

119899 (9)

where 119910119887max and 119910119887max denote the peak base displacements

for the fuzzy control and uncontrolled cases respectively119886119894max and 119886119894max represent the peak superstructure accelera-tion for the fuzzy control and uncontrolled case respectively

The objective of genetic algorithm is tomake the objectivefitness function reach its minimum value by selecting oneset of parameters of supervisory fuzzy control and preload

Mathematical Problems in Engineering 9

0

1

X

0

1

Deg

ree o

f mem

bers

hip

Deg

ree o

f mem

bers

hip

0

1

Deg

ree o

f mem

bers

hip

1205901

1205901 1205902 1205903

Rule 1 (1 6) Rule 1 (7 12) Rule 5 (24 30)middot middot middot

c1

c1 c2 c3

1205902

Y1

1205903

Y2c2 c3

Figure 10 Encoding structure for genetic algorithm

of piezoelectric friction damper The initial population sizegenetic algebra and crossover probability are set to 20 50and 08 respectively Through inputting the artificial earth-quakes which are characterized by near-fault earthquakesfor different ground sites the supervisory fuzzy control andpreload of piezoelectric friction dampers can be optimizedThe fuzzy control surfaces of optimized supervisory fuzzycontrol are shown in Figure 12

5 Linear Quadratic Gaussian Controller

LQG (Linear Quadratic Gaussian) method is based onKalman filter technique which has become a widely usedcontrol algorithm For comparison purpose LQG is adoptedto regulate the contact normal force of piezoelectric frictiondamper in the study The optimal controller takes groundacceleration as white noise and considers the velocity anddisplacement of base isolation as feedback signals Thecontrol performance index is defined as follows [22]

119869 = lim120591rarr+infin

1

120591

sdot 119864 int

120591

0

[Z (119905)119879QZ (119905) + U (119905)119879RU (119905)] 119889 (119905) (10)

where Q2119899times2119899

and R1times1

are semi-positive definite matrix andpositive definite matrix respectivelyThe control force can beobtained as follows

U (119905) = minusGZ (119905) (11)

G = Rminus1B119879P (12)

where P can be computed by the solution of the Riccatiequation as follows

minusPA minus A119879P + PBRminus1B119879P minusQ = 0 (13)

The control force obtained from the above equation isactive control force which could not be always achieved bypiezoelectric friction damper It is realized that the directionof active control force is opposite to the slipping direction ofpiezoelectric friction damper Therefore the desired controlforce119906

119889(119905) can be achieved according to the following criteria

119906119889(119905)

=

119891max sgn (119887) (119906active

119887lt 0

10038161003816100381610038161003816119906active10038161003816100381610038161003816 gt 119891max)

10038161003816100381610038161003816119906active10038161003816100381610038161003816 sgn (119887) (119906

active119887lt 0

10038161003816100381610038161003816119906active10038161003816100381610038161003816 le 119891max)

119891min sgn (119887) (119906active

119887ge 0)

(14)

10 Mathematical Problems in Engineering

Table 5 Parameters of base-isolated structure

Floor masses(kg)

Stiffness values(kNm)

Dampingcoefficients(kN sm)

Isolated floor 6800 232 745First floor 5897 33732 67Second floor 5897 29093 58Third floor 5897 28621 57Fourth floor 5897 24954 50Fifth floor 5897 19059 38

No

Yes

Encode

Generate initial random population

Calculate the value of fitness and rank

Copy crossover and mutation

Decode

Optimal solution

Whether or not to meet thecondition of convergence

Figure 11 Flow chart of genetic algorithm

where 119906active is the control force obtained from LQG con-troller

119887is the velocity of base isolator119891max and119891min are the

maximum and minimum friction forces of the piezoelectricfriction damper respectively

6 Numerical Simulations

61 Model of the Base-Isolated Structure A five-story base-isolated building which is proposed by He et al is employedto evaluate the performance of developed fuzzy controllers[18] The fundamental period of the five-story building is03 s For the given isolation parameters the fundamentalperiod of the base-isolated building becomes 25 sThereforean isolation ratio 120575 equal to 83 (=2503) is obtainedThe model of the base-isolated structure with piezoelectricfriction damper is shown in Figure 13 The parameters of thebase-isolated structure are shown in Table 5

62 Performance Evaluation Index In order to evaluate theperformance of base-isolated structure for different controlalgorithms a total of nine performance indexes are employedin this study [23] as shown in Table 6

The performance indexes J1through J

5denote the struc-

ture responses for the controlled building normalized byuncontrolled structure respectively The performance indexJ6evaluates the peak control force normalized by the peak

base shear for controlled structure The performance indexesJ7and J8represent RMS (Root Mean Square) base displace-

ments and RMS floor accelerations respectively J9computes

the energy dissipated by friction dampers normalized by theearthquake input energy to the controlled structure

63 Simulation Results and Analysis A total of nine seis-mic excitations that contain six real ground motions andthree artificial earthquakes are selected to evaluate the per-formance of the optimized fuzzy logic controller In thisstudy the time histories of strong earthquake which rangefrom 20 s to 70 s are selected for numerical simulation andanalysis

The numerical results for various earthquakes are listedin Table 7 In the table the Genetic Algorithm HierarchicFuzzy Logic Control is named as GHFLC Moreover forcomparison purpose the results for an optimal controller andpassive operation of friction damper are also listed in thetable Numbers in bold font indicate the best results amongall control cases

Base displacement is an important index to evaluatethe effectiveness for different controllers For a base-isolatedstructure the reduction of base displacement is a primarypurpose to prevent permanent damage for isolation bearingsor adjacent buildings Although passive operation of frictiondampers can successfully reduce the performance indexassociated with the peak and RMS base displacements (J

3and

J7) it causes significant amplification in peak and RMS floor

accelerations (J5and J

8) for most cases due to the passive

control For example as compared to the uncontrolledstructure for TCU052 TCU053 and TCU054 earthquakespassive control leads to 6 45 and 42 amplification inpeak floor acceleration respectively However the proposedfuzzy controller can successfully improve the base-isolatedstructure acceleration at the cost of slight deterioration in theperformance indices J

3and J7on comparison with passive

control For example for TCU052 TCU053 and TCU054earthquakes GHFLC results in 15 13 and 16 decrease inpeak floor accelerations respectively As compared to passivecontrol there are 9 3 and 7 increase in peak basedisplacements

The time histories of friction force and force-displacement curves of friction dampers for differentcontrollers subjected to TCU052 earthquake are shown inFigure 14 From the figures it can be seen that the passivecontrol outputs lager damper force than GHFLC Becausethe supervisory fuzzy control can alter input normalizationfactors of sublevel FLC according to the current level ofground motion there are some serrations presented at theedge of the hysteretic curve of piezoelectric friction damper

The comparison of the performance indexes J3 J7 J5and

J8under different control cases is shown in Figures 15 and

16 respectively From these figures it can be seen that thefuzzy controller is more effective than passive and optimal

Mathematical Problems in Engineering 11O

utpu

t

009

055

026

000033

000094000

Input ground velocity (ms)

Nd

N

(a) Hard soilO

utpu

t

Input ground velocity (ms)

071

042

000

008000

037

103000

Nd

N

(b) Medium soil

Out

put

Input ground velocity (ms)

107

053

000045

011000

117000

Nd

N

(c) Soft soil

Figure 12 Control surface for optimized supervisory fuzzy control

PFD

Fixed reference

LRB

Figure 13 Model of the base-isolated structure

12 Mathematical Problems in Engineering

Table 6 Performance index

Peak base shear Peak interstory drift RMS base displacement

1198691=max119905

10038171003817100381710038171198810 (119905)1003817100381710038171003817

max119905

100381710038171003817100381710038171198810(119905)10038171003817100381710038171003817

1198694=

max119905119891

10038171003817100381710038171003817119889119891(119905)10038171003817100381710038171003817

max119905119891

10038171003817100381710038171003817119889119891(119905)10038171003817100381710038171003817

1198697=

max119894

1003817100381710038171003817120590119889 (119905)1003817100381710038171003817

max119905

1003817100381710038171003817119889 (119905)1003817100381710038171003817

Peak structural shear Peak floor acceleration RMS floor acceleration

1198692=max119905

10038171003817100381710038171198811 (119905)1003817100381710038171003817

max119905

100381710038171003817100381710038171198811(119905)10038171003817100381710038171003817

1198695=

max119905119891

10038171003817100381710038171003817119886119891(119905)10038171003817100381710038171003817

max119905119891

10038171003817100381710038171003817119886119891(119905)10038171003817100381710038171003817

1198698=max119891

1003817100381710038171003817120590119886 (119905)1003817100381710038171003817

max119891

1003817100381710038171003817119886 (119905)1003817100381710038171003817

Peak base displacement Peak control force Energy dissipated by PFD

1198693=max119905

1003817100381710038171003817119909119887 (119905)1003817100381710038171003817

max119905

1003817100381710038171003817119909119887 (119905)1003817100381710038171003817

1198696=max119905

1003817100381710038171003817119891119889 (119905)1003817100381710038171003817

max119905

10038171003817100381710038171198810 (119905)1003817100381710038171003817

1198699=

int119879

0

119891119889(119905) 119887(119905) 119889119905

int119879

0

1198810(119905) 119892(119905) 119889119905

Table 7 Results of numerical simulation

Earthquake Control case 1198691

1198692

1198693

1198694

1198695

1198696

1198697

1198698

1198699

TCU102(hard site)

Passive 081 082 068 085 094 048 057 082 078Optimal 092 095 075 099 087 043 068 081 069GHFLC 087 091 071 093 082 041 061 078 073

TCU052(hard site)

Passive 079 079 046 082 106 036 038 089 087Optimal 087 087 057 087 098 029 049 085 079GHFLC 083 082 055 082 091 033 044 079 084

Artificialearthquake(hard site)

Passive 072 074 054 076 092 054 049 090 084Optimal 084 086 069 083 089 047 057 086 073GHFLC 076 077 061 079 083 042 052 081 076

TCU053(medium site)

Passive 061 065 039 071 145 032 037 116 089Optimal 069 072 046 076 136 031 045 117 078GHFLC 062 062 042 065 132 026 044 109 072

TCU054(medium site)

Passive 071 073 043 073 142 084 038 121 088Optimal 081 087 045 085 132 079 052 125 086GHFLC 075 071 040 074 126 082 045 113 076

Artificialearthquake(medium site)

Passive 054 057 038 064 123 067 036 117 091Optimal 067 066 047 067 119 078 048 113 079GHFLC 058 061 040 062 113 072 041 109 085

TCU110(soft soil site)

Passive 077 078 047 077 103 050 045 089 095Optimal 083 082 052 085 107 046 052 099 087GHFLC 086 086 056 086 104 042 049 093 090

CHY101(soft soil site)

Passive 069 071 058 075 086 066 054 092 084Optimal 075 073 062 074 087 064 055 088 079GHFLC 063 067 054 067 079 065 051 087 083

Artificialearthquake(soft site)

Passive 057 064 061 068 097 061 058 098 088Optimal 071 070 074 075 094 058 071 093 083GHFLC 065 062 067 069 085 055 063 086 076

controller in simultaneously depressing the superstructureacceleration and base displacement For example the appli-cation of developed fuzzy controller leads to an average of112 decrease in peak floor acceleration and an average ofonly 36 increase in peak base displacement as compared topassive control Particularly optimal controller produces anaverage of only 41 reduction in peak floor acceleration and

leads to 79 increase in peak base displacement as comparedto passive control Therefore the improved fuzzy controlmethod shows better performance than passive and optimalcontrol

In order to further evaluate the performance of differentcontrollers the energy time histories for different controllersare compared with each other For a base-isolated structure

Mathematical Problems in Engineering 13

20 30 40 50 60 70minus20

minus10

00

10

20Fr

ictio

n fo

rce (

kN)

Time (s)minus03 minus02 minus01 00 01 02 03

minus20

minus10

00

10

20

Fric

tion

forc

e (kN

)

Displacement (m)

(a) Passive control

20 30 40 50 60 70minus20

minus10

00

10

20

Fric

tion

forc

e (kN

)

Time (s)minus03 minus02 minus01 00 01 02 03

minus20

minus10

00

10

20

Fric

tion

forc

e (kN

)

Displacement (m)

(b) GHFLC method

Figure 14 Time histories of friction force and force-displacement diagram against TCU052 earthquake

1 2 3 4 5 6 7 8 903

04

05

06

07

08

Excitation case

Passive OptimalGHFLC

1 2 3 4 5 6 7 8 903

04

05

06

07

Excitation casePassive

GHFLC Optimal

J 3 J 5

Figure 15 Comparisons on the performance indexes J3and J7for different control cases

14 Mathematical Problems in Engineering

1 2 3 4 5 6 7 8 907

08

09

10

11

12

13

14

15

Excitation casePassive

GHFLC Optimal

1 2 3 4 5 6 7 8 907

08

09

10

11

12

13

Excitation case

Passive

GHFLC Optimal

J 8J 5

Figure 16 Comparison of the performance indexes J5and J8for different control cases

with piezoelectric friction dampers installed on the isolationthe energy equations are defined as follows

119864119870+ 119864120585+ 119864119878+ 119864119867= 119864119868

119864119870=1

2119879

119905119872119905

119864120585= int

119905

0

119879

119888 119889119905

119864119878= int

119905

0

119909119879

119870119889119909

119864119867= minusint

119905

0

119906119879

119864119879

119904119889119909

119864119868= minusint

119905

0

gMI 119889119909

(15)

where 119864119870 119864120585 119864119878 119864119867 and 119864

119868denote the absolute kinetic

energy damping energy elastic strain energy energy dis-sipated by piezoelectric friction dampers and total inputenergy respectively The energy time histories for differentcontrollers against TCU052Chi-Chi earthquake are shown inFigure 17 It can be seen from the figures that the piezoelectricfriction dampers dissipate most of the input energy fordifferent control cases subjected to TCU052 earthquake

In order to compare different effects under near-faultground motions recorded for different sites the average ofinput energy and structure responses subjected to near-faultearthquakes are given in Table 8

As shown in Table 8 the near-fault earthquakes forsoft sites are more destructive than hard sites For instancecompared to hard sites the input energy and the base dis-placement of RMS of the base-isolated structure for soft soil

increase by 143 and 256 respectively However GHFLCpossesses favorable performance under different ground sitesand the damping effect has no distinctly direct relationshipwith site category

As discussed in Section 61 the isolation ratio of thesimulation model equals 83 In order to evaluate the effectsof isolation ratio on the damping performance of GHFLC thestiffness value of isolation is adjusted to 1045 and 452 kNmrespectively Then the numerical results for different valuesof isolation ratio (120575 = 4 6) are obtained The performanceindexes J

3and J5for different isolation ratios are shown in

Figures 18 and 19 respectivelyFor base-isolated structure isolation ratio has a signifi-

cant influence on the isolation effect A larger isolation ratiowhich means a minor stiffness value of isolation usuallyleads to conspicuous enlargement of base displacement anddecrease of superstructural responses due to the increaseof fundamental vibration period and vice versa Howeveras shown in Figures 18 and 19 the shock absorption rateof GHFLC has little change when isolation ratio variesdifferently and the proposed fuzzy control shows favorableeffectiveness in the diverse isolation ratios of base-isolatedstructures

7 Conclusions

In this study an optimized fuzzy logic control which isdesigned for Chi-Chi near-fault earthquakes under differentground sites is proposed An elastic design spectrum isproposed to generate near-fault earthquakes for differentground sitesThe characteristic of the design spectrum is thatit has larger periods and peak acceleration than conventionalspectrum Genetic algorithm is employed to optimize thesupervisory fuzzy controller and preload of piezoelectric

Mathematical Problems in Engineering 15

Table 8 Average ofinput energy and structure responses subjected to near-fault earthquakes

Site classification Input energy (kNsdotm) Base shear (kN) Base displacement ofRMS (m)

Structure accelerationof RMS (g)

Hard soil 24375 475 0047 0432Medium soil 26746 498 0054 0476Soft soil 27857 568 0059 0531

20 30 40 50 60 7000

05

10

15

20

25

Input energyEnergy dissipated by dampers

Time (s)

Ener

gy (k

Nmiddotm

)

times104

(a) Passive control

20 30 40 50 60 7000

05

10

15

20

25

30

Time (s)

Input energyEnergy dissipated by dampers

Ener

gy (k

Nmiddotm

)

times104

(b) Optimal control

20 30 40 50 60 7000

05

10

15

20

25

30

Input energyEnergy dissipated by dampers

Time (s)

Ener

gy (k

Nmiddotm

)

times104

(c) GHFLC method

Figure 17 Energy time histories subjected to Chi-Chi TCU052 earthquake

friction dampers according to three artificial earthquakesthat are characterized by Chi-Chi earthquakes Passive andoptimal controllers are also compared with the performanceof the developed fuzzy controller The simulation resultsreveal that the developed semiactive fuzzy controller hasbetter performance than traditional passive and optimal con-troller in simultaneously reducing the base displacement and

floor acceleration under near-fault earthquakes for differentground sites

Conflict of Interests

The authors declare no conflict of interests regarding thepublication of this paper

16 Mathematical Problems in Engineering

1 2 3 4 5 6 7 8 903

04

05

06

07

08

Excitation casePassive

GHFLC Optimal

1 2 3 4 5 6 7 8 907

08

09

10

11

12

13

14

15

Excitation case

Passive

GHFLC Optimal

J 3 J 5Figure 18 Comparisons on the performance indexes J

3and J5for different control cases (120575 = 4)

1 2 3 4 5 6 7 8 903

04

05

06

07

08

Excitation casePassive

GHFLC Optimal

1 2 3 4 5 6 7 8 907

08

09

10

11

12

13

14

15

Excitation casePassive

GHFLC Optimal

J 3 J 5

Figure 19 Comparisons on the performance indexes J3and J5for different control cases (120575 = 6)

Acknowledgments

This research was supported by National Natural ScienceFoundation of China under Grant no 51308487 no 41402261and no 51408526 Hebei Provincial Natural Science Founda-tion ofChina underGrant no E2014203055 and the ExcellentYouth Foundation of Hebei Educational Committee underGrant no YQ2013015 The support for this research is greatlyappreciated

References

[1] C Alhan and H Gavin ldquoA parametric study of linear and non-linear passively damped seismic isolation systems for buildingsrdquoEngineering Structures vol 26 no 4 pp 485ndash497 2004

[2] R S Jangid and J M Kelly ldquoBase isolation for near-faultmotionsrdquoEarthquake Engineering and Structural Dynamics vol30 no 5 pp 691ndash707 2001

[3] J Shen M-H Tsai K-C Chang and G C Lee ldquoPerformanceof a seismically isolated bridge under near-fault earthquake

Mathematical Problems in Engineering 17

ground motionsrdquo Journal of Structural Engineering vol 130 no6 pp 861ndash868 2004

[4] F Mazza A Vulcano and M Mazza ldquoNonlinear dynamicresponse of RC buildings with different base Isolation systemssubjected to horizontal and vertical components of near-faultground motionsrdquo Open Construction and Building TechnologyJournal vol 6 pp 373ndash383 2012

[5] F Mazza and A Vulcano ldquoEffects of near-fault ground motionson the nonlinear dynamic response of base-isolated rc framedbuildingsrdquo Earthquake Engineering and Structural Dynamicsvol 41 no 2 pp 211ndash232 2012

[6] O E Ozbulut and S Hurlebaus ldquoFuzzy control of piezoelectricfriction dampers for seismic protection of smart base isolatedbuildingsrdquo Bulletin of Earthquake Engineering vol 8 no 6 pp1435ndash1455 2010

[7] O E Ozbulut M Bitaraf and S Hurlebaus ldquoAdaptive controlof base-isolated structures against near-field earthquakes usingvariable friction dampersrdquo Engineering Structures vol 33 no12 pp 3143ndash3154 2011

[8] J M Kelly ldquoThe role of damping in seismic isolationrdquo Earth-quake Engineering and Structural Dynamics vol 28 no 1 pp3ndash20 1999

[9] F Mazza and A Vulcano ldquoNonlinear response of RC framedbuildings with isolation and supplemental damping at the basesubjected to near-fault earthquakesrdquo Journal of EarthquakeEngineering vol 13 no 5 pp 690ndash715 2009

[10] M Bitaraf and S Hurlebaus ldquoSemi-active adaptive control ofseismically excited 20-story nonlinear buildingrdquo EngineeringStructures vol 56 no 11 pp 2107ndash2118 2013

[11] D Das T K Datta and A Madan ldquoSemiactive fuzzy controlof the seismic response of building frames with MR dampersrdquoEarthquake Engineering and Structural Dynamics vol 41 no 1pp 99ndash118 2012

[12] A-P Wang and C-D Lee ldquoFuzzy sliding mode control for abuilding structure based on genetic algorithmsrdquo EarthquakeEngineering and Structural Dynamics vol 31 no 4 pp 881ndash8952002

[13] D G Reigles and M D Symans ldquoSupervisory fuzzy controlof a base-isolated benchmark building utilizing a neuro-fuzzymodel of controllable fluid viscous dampersrdquo Structural Controland Health Monitoring vol 13 no 2-3 pp 724ndash747 2006

[14] H-S Kim and P N Roschke ldquoGA-fuzzy control of smartbase isolated benchmark building using supervisory controltechniquerdquo Advances in Engineering Software vol 38 no 7 pp453ndash465 2007

[15] D Yang and Y Zhao ldquoEffects of rupture forward directivity andfling step of near-fault groundmotions on seismic performanceof base-isolated building structurerdquo Acta Seismologica Sinicavol 32 no 5 pp 579ndash587 2010

[16] Y E-A Mohamedzein J A Abdalla and A Abdelwahab ldquoSiteresponse and earthquake design spectra for central KhartoumSudanrdquoBulletin of Earthquake Engineering vol 4 no 3 pp 277ndash293 2006

[17] D Zhao and H Li ldquoShaking table tests and analyses of semi-active fuzzy control for structural seismic reduction with apiezoelectric variable-friction damperrdquo Smart Materials andStructures vol 19 no 10 Article ID 105031 2010

[18] W L He A K Agrawal and J N Yang ldquoNovel semiactivefriction controller for linear structures against earthquakesrdquoJournal of Structural Engineering vol 129 no 7 pp 941ndash9502003

[19] J N Yang and A K Agrawal ldquoSemi-active hybrid controlsystems for nonlinear buildings against near-field earthquakesrdquoEngineering Structures vol 24 no 3 pp 271ndash280 2002

[20] O E Ozbulut and S Hurlebaus ldquoOptimal design of supere-lastic-friction base isolators for seismic protection of highwaybridges against near-field earthquakesrdquo Earthquake Engineeringand Structural Dynamics vol 40 no 3 pp 273ndash291 2011

[21] D A Shook P N Roschke and O E Ozbulut ldquoSuperelasticsemi-active damping of a base-isolated structurerdquo StructuralControl and HealthMonitoring vol 15 no 5 pp 746ndash768 2008

[22] K D PhamG JinM K Sain B F Spencer Jr and S R LibertyldquoGeneralized linear quadratic Gaussian techniques for the windbenchmark problemrdquo Journal of Engineering Mechanics vol130 no 4 pp 466ndash470 2004

[23] S Nagarajaiah and S Narasimhan ldquoSmart base-isolated bench-mark building Part II Phase I sample controllers for linearisolation systemsrdquo Structural Control and Health Monitoringvol 13 no 2-3 pp 605ndash625 2006

Submit your manuscripts athttpwwwhindawicom

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

MathematicsJournal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Mathematical Problems in Engineering

Hindawi Publishing Corporationhttpwwwhindawicom

Differential EquationsInternational Journal of

Volume 2014

Applied MathematicsJournal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Probability and StatisticsHindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Journal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Mathematical PhysicsAdvances in

Complex AnalysisJournal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

OptimizationJournal of

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CombinatoricsHindawi Publishing Corporationhttpwwwhindawicom Volume 2014

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Operations ResearchAdvances in

Journal of

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Function Spaces

Abstract and Applied AnalysisHindawi Publishing Corporationhttpwwwhindawicom Volume 2014

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Discrete Dynamics in Nature and Society

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

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Decision SciencesAdvances in

Discrete MathematicsJournal of

Hindawi Publishing Corporationhttpwwwhindawicom

Volume 2014 Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Stochastic AnalysisInternational Journal of

8 Mathematical Problems in Engineering

Table 4 Fuzzy control rules adopted for sublevel fuzzy control

Velocity ofisolated floor

Displacement of isolated floorNL NM NS ZE PS PM PL

NL VL VL L L M S ZENM VL L L M S ZE SNS L L M S ZE S MZE L M S ZE S M LPS M S ZE S M L LPM S ZE S M L L VLPL ZE S M L L VL VL

minus1minus05

005

1

minus1minus05

005

1

500

1000

VelocityDisplacement

Volta

ge (V

)

Figure 9 Fuzzy control surface for sublevel fuzzy controller

about zero this means that piezoelectric friction damper actsas a passive friction damper The defuzzification of fuzzycontrol adopts the method of centroid to get a crisp outputvalue The control surface and color-filled contour line ofsublevel fuzzy control are depicted in Figure 9

43 Supervisory Fuzzy Logic Controller In the fuzzy logiccontrol normalization factors need to satisfy a certain objec-tive The oversize normalization factors can enlarge the basedisplacement effectively Contrarily too small normalizationfactors can result in large control force that amplifies theaccelerations of base-isolated structure Thus a supervisoryfuzzy logic control is proposed to adjust its normalizationfactors in real-time As discussed earlier near-fault earth-quakes usually have long duration pulses with peak velocitiesThus the supervisory fuzzy control employs ground velocityas single input variable to identify the characteristics ofthe ground motion The normalization factors of sublevelfuzzy control are selected as two output variables HereGaussian membership functions are used for input andoutput variables as shown in

120583gauss = exp[minus(119909 minus 119888)2

21205902] (7)

where 119888 and 120590 are the constant values that define the shape ofthe Gauss functions respectively

The rules of the supervisory fuzzy controller are definedby the following form

Rule119894 IF 119883 is 119860119894 then 1198841is 1198621198941 1198842is 1198621198942

119894 = 1 2 119872

(8)

where119872 is the number of fuzzy control rules 119883 is the inputvariable 119884

1and 119884

2are the output variables 119860119894 119862119894

1 and 119862119894

2

are the linguistic values characterized by input and outputmembership functions respectively One fuzzy control ruleis described by three Gaussian membership functions andeach membership function can be defined by two parameters(119888 and 120590) Therefore a total of five fuzzy control rules canbe optimized by encoding these two parameters into thegene using genetic algorithm Consequently a total of 30parameters are encoded into the chromosome to define theinference system of supervisory fuzzy controller as shown inFigure 10

Similar to normalization factors the preload of thepiezoelectric friction dampers has a great influence on thedamping effect Thus it is essential to establish an effectivesupervisory fuzzy logic controller and a suitable preloadof piezoelectric friction damper Generally for the seismicprotection of a base-isolated structure there is a trade-off between the isolation displacement and superstructureacceleration The main control objective is to depress theisolation displacementwithout excessively increasing acceler-ation response of the superstructure In this section a geneticalgorithm is employed to seek out an optimal solution forthe control of the base-isolated structure The flow chart ofgenetic algorithm is shown in Figure 11

Genetic algorithm is a computational model for thesimulation of Darwin natural genetic selection and biologicalevolution Different from the traditional search algorithmgenetic algorithm begins to search a group of optimal solu-tions from an initial random population by mutation andrecombination Each individual which consists of a set ofbinary strings is a solution to the objective problem Afterinitialization genetic algorithm uses a sort method to rankindividuals It compares each solution with other solutionsin the population to find whether it is dominated Duringthe process of creating a new generation it selects a suitableindividual according to the size of the fitness value Afterseveral generations the individual value gradually convergesto the best chromosome which is the optimal solution

The objective fitness function employed in this study isshown as follows

119869 = 06 times119910119887max

119910119887max

+ 04 timesradicsum119899

119894=1(119886119894max119886119894max)

2

119899 (9)

where 119910119887max and 119910119887max denote the peak base displacements

for the fuzzy control and uncontrolled cases respectively119886119894max and 119886119894max represent the peak superstructure accelera-tion for the fuzzy control and uncontrolled case respectively

The objective of genetic algorithm is tomake the objectivefitness function reach its minimum value by selecting oneset of parameters of supervisory fuzzy control and preload

Mathematical Problems in Engineering 9

0

1

X

0

1

Deg

ree o

f mem

bers

hip

Deg

ree o

f mem

bers

hip

0

1

Deg

ree o

f mem

bers

hip

1205901

1205901 1205902 1205903

Rule 1 (1 6) Rule 1 (7 12) Rule 5 (24 30)middot middot middot

c1

c1 c2 c3

1205902

Y1

1205903

Y2c2 c3

Figure 10 Encoding structure for genetic algorithm

of piezoelectric friction damper The initial population sizegenetic algebra and crossover probability are set to 20 50and 08 respectively Through inputting the artificial earth-quakes which are characterized by near-fault earthquakesfor different ground sites the supervisory fuzzy control andpreload of piezoelectric friction dampers can be optimizedThe fuzzy control surfaces of optimized supervisory fuzzycontrol are shown in Figure 12

5 Linear Quadratic Gaussian Controller

LQG (Linear Quadratic Gaussian) method is based onKalman filter technique which has become a widely usedcontrol algorithm For comparison purpose LQG is adoptedto regulate the contact normal force of piezoelectric frictiondamper in the study The optimal controller takes groundacceleration as white noise and considers the velocity anddisplacement of base isolation as feedback signals Thecontrol performance index is defined as follows [22]

119869 = lim120591rarr+infin

1

120591

sdot 119864 int

120591

0

[Z (119905)119879QZ (119905) + U (119905)119879RU (119905)] 119889 (119905) (10)

where Q2119899times2119899

and R1times1

are semi-positive definite matrix andpositive definite matrix respectivelyThe control force can beobtained as follows

U (119905) = minusGZ (119905) (11)

G = Rminus1B119879P (12)

where P can be computed by the solution of the Riccatiequation as follows

minusPA minus A119879P + PBRminus1B119879P minusQ = 0 (13)

The control force obtained from the above equation isactive control force which could not be always achieved bypiezoelectric friction damper It is realized that the directionof active control force is opposite to the slipping direction ofpiezoelectric friction damper Therefore the desired controlforce119906

119889(119905) can be achieved according to the following criteria

119906119889(119905)

=

119891max sgn (119887) (119906active

119887lt 0

10038161003816100381610038161003816119906active10038161003816100381610038161003816 gt 119891max)

10038161003816100381610038161003816119906active10038161003816100381610038161003816 sgn (119887) (119906

active119887lt 0

10038161003816100381610038161003816119906active10038161003816100381610038161003816 le 119891max)

119891min sgn (119887) (119906active

119887ge 0)

(14)

10 Mathematical Problems in Engineering

Table 5 Parameters of base-isolated structure

Floor masses(kg)

Stiffness values(kNm)

Dampingcoefficients(kN sm)

Isolated floor 6800 232 745First floor 5897 33732 67Second floor 5897 29093 58Third floor 5897 28621 57Fourth floor 5897 24954 50Fifth floor 5897 19059 38

No

Yes

Encode

Generate initial random population

Calculate the value of fitness and rank

Copy crossover and mutation

Decode

Optimal solution

Whether or not to meet thecondition of convergence

Figure 11 Flow chart of genetic algorithm

where 119906active is the control force obtained from LQG con-troller

119887is the velocity of base isolator119891max and119891min are the

maximum and minimum friction forces of the piezoelectricfriction damper respectively

6 Numerical Simulations

61 Model of the Base-Isolated Structure A five-story base-isolated building which is proposed by He et al is employedto evaluate the performance of developed fuzzy controllers[18] The fundamental period of the five-story building is03 s For the given isolation parameters the fundamentalperiod of the base-isolated building becomes 25 sThereforean isolation ratio 120575 equal to 83 (=2503) is obtainedThe model of the base-isolated structure with piezoelectricfriction damper is shown in Figure 13 The parameters of thebase-isolated structure are shown in Table 5

62 Performance Evaluation Index In order to evaluate theperformance of base-isolated structure for different controlalgorithms a total of nine performance indexes are employedin this study [23] as shown in Table 6

The performance indexes J1through J

5denote the struc-

ture responses for the controlled building normalized byuncontrolled structure respectively The performance indexJ6evaluates the peak control force normalized by the peak

base shear for controlled structure The performance indexesJ7and J8represent RMS (Root Mean Square) base displace-

ments and RMS floor accelerations respectively J9computes

the energy dissipated by friction dampers normalized by theearthquake input energy to the controlled structure

63 Simulation Results and Analysis A total of nine seis-mic excitations that contain six real ground motions andthree artificial earthquakes are selected to evaluate the per-formance of the optimized fuzzy logic controller In thisstudy the time histories of strong earthquake which rangefrom 20 s to 70 s are selected for numerical simulation andanalysis

The numerical results for various earthquakes are listedin Table 7 In the table the Genetic Algorithm HierarchicFuzzy Logic Control is named as GHFLC Moreover forcomparison purpose the results for an optimal controller andpassive operation of friction damper are also listed in thetable Numbers in bold font indicate the best results amongall control cases

Base displacement is an important index to evaluatethe effectiveness for different controllers For a base-isolatedstructure the reduction of base displacement is a primarypurpose to prevent permanent damage for isolation bearingsor adjacent buildings Although passive operation of frictiondampers can successfully reduce the performance indexassociated with the peak and RMS base displacements (J

3and

J7) it causes significant amplification in peak and RMS floor

accelerations (J5and J

8) for most cases due to the passive

control For example as compared to the uncontrolledstructure for TCU052 TCU053 and TCU054 earthquakespassive control leads to 6 45 and 42 amplification inpeak floor acceleration respectively However the proposedfuzzy controller can successfully improve the base-isolatedstructure acceleration at the cost of slight deterioration in theperformance indices J

3and J7on comparison with passive

control For example for TCU052 TCU053 and TCU054earthquakes GHFLC results in 15 13 and 16 decrease inpeak floor accelerations respectively As compared to passivecontrol there are 9 3 and 7 increase in peak basedisplacements

The time histories of friction force and force-displacement curves of friction dampers for differentcontrollers subjected to TCU052 earthquake are shown inFigure 14 From the figures it can be seen that the passivecontrol outputs lager damper force than GHFLC Becausethe supervisory fuzzy control can alter input normalizationfactors of sublevel FLC according to the current level ofground motion there are some serrations presented at theedge of the hysteretic curve of piezoelectric friction damper

The comparison of the performance indexes J3 J7 J5and

J8under different control cases is shown in Figures 15 and

16 respectively From these figures it can be seen that thefuzzy controller is more effective than passive and optimal

Mathematical Problems in Engineering 11O

utpu

t

009

055

026

000033

000094000

Input ground velocity (ms)

Nd

N

(a) Hard soilO

utpu

t

Input ground velocity (ms)

071

042

000

008000

037

103000

Nd

N

(b) Medium soil

Out

put

Input ground velocity (ms)

107

053

000045

011000

117000

Nd

N

(c) Soft soil

Figure 12 Control surface for optimized supervisory fuzzy control

PFD

Fixed reference

LRB

Figure 13 Model of the base-isolated structure

12 Mathematical Problems in Engineering

Table 6 Performance index

Peak base shear Peak interstory drift RMS base displacement

1198691=max119905

10038171003817100381710038171198810 (119905)1003817100381710038171003817

max119905

100381710038171003817100381710038171198810(119905)10038171003817100381710038171003817

1198694=

max119905119891

10038171003817100381710038171003817119889119891(119905)10038171003817100381710038171003817

max119905119891

10038171003817100381710038171003817119889119891(119905)10038171003817100381710038171003817

1198697=

max119894

1003817100381710038171003817120590119889 (119905)1003817100381710038171003817

max119905

1003817100381710038171003817119889 (119905)1003817100381710038171003817

Peak structural shear Peak floor acceleration RMS floor acceleration

1198692=max119905

10038171003817100381710038171198811 (119905)1003817100381710038171003817

max119905

100381710038171003817100381710038171198811(119905)10038171003817100381710038171003817

1198695=

max119905119891

10038171003817100381710038171003817119886119891(119905)10038171003817100381710038171003817

max119905119891

10038171003817100381710038171003817119886119891(119905)10038171003817100381710038171003817

1198698=max119891

1003817100381710038171003817120590119886 (119905)1003817100381710038171003817

max119891

1003817100381710038171003817119886 (119905)1003817100381710038171003817

Peak base displacement Peak control force Energy dissipated by PFD

1198693=max119905

1003817100381710038171003817119909119887 (119905)1003817100381710038171003817

max119905

1003817100381710038171003817119909119887 (119905)1003817100381710038171003817

1198696=max119905

1003817100381710038171003817119891119889 (119905)1003817100381710038171003817

max119905

10038171003817100381710038171198810 (119905)1003817100381710038171003817

1198699=

int119879

0

119891119889(119905) 119887(119905) 119889119905

int119879

0

1198810(119905) 119892(119905) 119889119905

Table 7 Results of numerical simulation

Earthquake Control case 1198691

1198692

1198693

1198694

1198695

1198696

1198697

1198698

1198699

TCU102(hard site)

Passive 081 082 068 085 094 048 057 082 078Optimal 092 095 075 099 087 043 068 081 069GHFLC 087 091 071 093 082 041 061 078 073

TCU052(hard site)

Passive 079 079 046 082 106 036 038 089 087Optimal 087 087 057 087 098 029 049 085 079GHFLC 083 082 055 082 091 033 044 079 084

Artificialearthquake(hard site)

Passive 072 074 054 076 092 054 049 090 084Optimal 084 086 069 083 089 047 057 086 073GHFLC 076 077 061 079 083 042 052 081 076

TCU053(medium site)

Passive 061 065 039 071 145 032 037 116 089Optimal 069 072 046 076 136 031 045 117 078GHFLC 062 062 042 065 132 026 044 109 072

TCU054(medium site)

Passive 071 073 043 073 142 084 038 121 088Optimal 081 087 045 085 132 079 052 125 086GHFLC 075 071 040 074 126 082 045 113 076

Artificialearthquake(medium site)

Passive 054 057 038 064 123 067 036 117 091Optimal 067 066 047 067 119 078 048 113 079GHFLC 058 061 040 062 113 072 041 109 085

TCU110(soft soil site)

Passive 077 078 047 077 103 050 045 089 095Optimal 083 082 052 085 107 046 052 099 087GHFLC 086 086 056 086 104 042 049 093 090

CHY101(soft soil site)

Passive 069 071 058 075 086 066 054 092 084Optimal 075 073 062 074 087 064 055 088 079GHFLC 063 067 054 067 079 065 051 087 083

Artificialearthquake(soft site)

Passive 057 064 061 068 097 061 058 098 088Optimal 071 070 074 075 094 058 071 093 083GHFLC 065 062 067 069 085 055 063 086 076

controller in simultaneously depressing the superstructureacceleration and base displacement For example the appli-cation of developed fuzzy controller leads to an average of112 decrease in peak floor acceleration and an average ofonly 36 increase in peak base displacement as compared topassive control Particularly optimal controller produces anaverage of only 41 reduction in peak floor acceleration and

leads to 79 increase in peak base displacement as comparedto passive control Therefore the improved fuzzy controlmethod shows better performance than passive and optimalcontrol

In order to further evaluate the performance of differentcontrollers the energy time histories for different controllersare compared with each other For a base-isolated structure

Mathematical Problems in Engineering 13

20 30 40 50 60 70minus20

minus10

00

10

20Fr

ictio

n fo

rce (

kN)

Time (s)minus03 minus02 minus01 00 01 02 03

minus20

minus10

00

10

20

Fric

tion

forc

e (kN

)

Displacement (m)

(a) Passive control

20 30 40 50 60 70minus20

minus10

00

10

20

Fric

tion

forc

e (kN

)

Time (s)minus03 minus02 minus01 00 01 02 03

minus20

minus10

00

10

20

Fric

tion

forc

e (kN

)

Displacement (m)

(b) GHFLC method

Figure 14 Time histories of friction force and force-displacement diagram against TCU052 earthquake

1 2 3 4 5 6 7 8 903

04

05

06

07

08

Excitation case

Passive OptimalGHFLC

1 2 3 4 5 6 7 8 903

04

05

06

07

Excitation casePassive

GHFLC Optimal

J 3 J 5

Figure 15 Comparisons on the performance indexes J3and J7for different control cases

14 Mathematical Problems in Engineering

1 2 3 4 5 6 7 8 907

08

09

10

11

12

13

14

15

Excitation casePassive

GHFLC Optimal

1 2 3 4 5 6 7 8 907

08

09

10

11

12

13

Excitation case

Passive

GHFLC Optimal

J 8J 5

Figure 16 Comparison of the performance indexes J5and J8for different control cases

with piezoelectric friction dampers installed on the isolationthe energy equations are defined as follows

119864119870+ 119864120585+ 119864119878+ 119864119867= 119864119868

119864119870=1

2119879

119905119872119905

119864120585= int

119905

0

119879

119888 119889119905

119864119878= int

119905

0

119909119879

119870119889119909

119864119867= minusint

119905

0

119906119879

119864119879

119904119889119909

119864119868= minusint

119905

0

gMI 119889119909

(15)

where 119864119870 119864120585 119864119878 119864119867 and 119864

119868denote the absolute kinetic

energy damping energy elastic strain energy energy dis-sipated by piezoelectric friction dampers and total inputenergy respectively The energy time histories for differentcontrollers against TCU052Chi-Chi earthquake are shown inFigure 17 It can be seen from the figures that the piezoelectricfriction dampers dissipate most of the input energy fordifferent control cases subjected to TCU052 earthquake

In order to compare different effects under near-faultground motions recorded for different sites the average ofinput energy and structure responses subjected to near-faultearthquakes are given in Table 8

As shown in Table 8 the near-fault earthquakes forsoft sites are more destructive than hard sites For instancecompared to hard sites the input energy and the base dis-placement of RMS of the base-isolated structure for soft soil

increase by 143 and 256 respectively However GHFLCpossesses favorable performance under different ground sitesand the damping effect has no distinctly direct relationshipwith site category

As discussed in Section 61 the isolation ratio of thesimulation model equals 83 In order to evaluate the effectsof isolation ratio on the damping performance of GHFLC thestiffness value of isolation is adjusted to 1045 and 452 kNmrespectively Then the numerical results for different valuesof isolation ratio (120575 = 4 6) are obtained The performanceindexes J

3and J5for different isolation ratios are shown in

Figures 18 and 19 respectivelyFor base-isolated structure isolation ratio has a signifi-

cant influence on the isolation effect A larger isolation ratiowhich means a minor stiffness value of isolation usuallyleads to conspicuous enlargement of base displacement anddecrease of superstructural responses due to the increaseof fundamental vibration period and vice versa Howeveras shown in Figures 18 and 19 the shock absorption rateof GHFLC has little change when isolation ratio variesdifferently and the proposed fuzzy control shows favorableeffectiveness in the diverse isolation ratios of base-isolatedstructures

7 Conclusions

In this study an optimized fuzzy logic control which isdesigned for Chi-Chi near-fault earthquakes under differentground sites is proposed An elastic design spectrum isproposed to generate near-fault earthquakes for differentground sitesThe characteristic of the design spectrum is thatit has larger periods and peak acceleration than conventionalspectrum Genetic algorithm is employed to optimize thesupervisory fuzzy controller and preload of piezoelectric

Mathematical Problems in Engineering 15

Table 8 Average ofinput energy and structure responses subjected to near-fault earthquakes

Site classification Input energy (kNsdotm) Base shear (kN) Base displacement ofRMS (m)

Structure accelerationof RMS (g)

Hard soil 24375 475 0047 0432Medium soil 26746 498 0054 0476Soft soil 27857 568 0059 0531

20 30 40 50 60 7000

05

10

15

20

25

Input energyEnergy dissipated by dampers

Time (s)

Ener

gy (k

Nmiddotm

)

times104

(a) Passive control

20 30 40 50 60 7000

05

10

15

20

25

30

Time (s)

Input energyEnergy dissipated by dampers

Ener

gy (k

Nmiddotm

)

times104

(b) Optimal control

20 30 40 50 60 7000

05

10

15

20

25

30

Input energyEnergy dissipated by dampers

Time (s)

Ener

gy (k

Nmiddotm

)

times104

(c) GHFLC method

Figure 17 Energy time histories subjected to Chi-Chi TCU052 earthquake

friction dampers according to three artificial earthquakesthat are characterized by Chi-Chi earthquakes Passive andoptimal controllers are also compared with the performanceof the developed fuzzy controller The simulation resultsreveal that the developed semiactive fuzzy controller hasbetter performance than traditional passive and optimal con-troller in simultaneously reducing the base displacement and

floor acceleration under near-fault earthquakes for differentground sites

Conflict of Interests

The authors declare no conflict of interests regarding thepublication of this paper

16 Mathematical Problems in Engineering

1 2 3 4 5 6 7 8 903

04

05

06

07

08

Excitation casePassive

GHFLC Optimal

1 2 3 4 5 6 7 8 907

08

09

10

11

12

13

14

15

Excitation case

Passive

GHFLC Optimal

J 3 J 5Figure 18 Comparisons on the performance indexes J

3and J5for different control cases (120575 = 4)

1 2 3 4 5 6 7 8 903

04

05

06

07

08

Excitation casePassive

GHFLC Optimal

1 2 3 4 5 6 7 8 907

08

09

10

11

12

13

14

15

Excitation casePassive

GHFLC Optimal

J 3 J 5

Figure 19 Comparisons on the performance indexes J3and J5for different control cases (120575 = 6)

Acknowledgments

This research was supported by National Natural ScienceFoundation of China under Grant no 51308487 no 41402261and no 51408526 Hebei Provincial Natural Science Founda-tion ofChina underGrant no E2014203055 and the ExcellentYouth Foundation of Hebei Educational Committee underGrant no YQ2013015 The support for this research is greatlyappreciated

References

[1] C Alhan and H Gavin ldquoA parametric study of linear and non-linear passively damped seismic isolation systems for buildingsrdquoEngineering Structures vol 26 no 4 pp 485ndash497 2004

[2] R S Jangid and J M Kelly ldquoBase isolation for near-faultmotionsrdquoEarthquake Engineering and Structural Dynamics vol30 no 5 pp 691ndash707 2001

[3] J Shen M-H Tsai K-C Chang and G C Lee ldquoPerformanceof a seismically isolated bridge under near-fault earthquake

Mathematical Problems in Engineering 17

ground motionsrdquo Journal of Structural Engineering vol 130 no6 pp 861ndash868 2004

[4] F Mazza A Vulcano and M Mazza ldquoNonlinear dynamicresponse of RC buildings with different base Isolation systemssubjected to horizontal and vertical components of near-faultground motionsrdquo Open Construction and Building TechnologyJournal vol 6 pp 373ndash383 2012

[5] F Mazza and A Vulcano ldquoEffects of near-fault ground motionson the nonlinear dynamic response of base-isolated rc framedbuildingsrdquo Earthquake Engineering and Structural Dynamicsvol 41 no 2 pp 211ndash232 2012

[6] O E Ozbulut and S Hurlebaus ldquoFuzzy control of piezoelectricfriction dampers for seismic protection of smart base isolatedbuildingsrdquo Bulletin of Earthquake Engineering vol 8 no 6 pp1435ndash1455 2010

[7] O E Ozbulut M Bitaraf and S Hurlebaus ldquoAdaptive controlof base-isolated structures against near-field earthquakes usingvariable friction dampersrdquo Engineering Structures vol 33 no12 pp 3143ndash3154 2011

[8] J M Kelly ldquoThe role of damping in seismic isolationrdquo Earth-quake Engineering and Structural Dynamics vol 28 no 1 pp3ndash20 1999

[9] F Mazza and A Vulcano ldquoNonlinear response of RC framedbuildings with isolation and supplemental damping at the basesubjected to near-fault earthquakesrdquo Journal of EarthquakeEngineering vol 13 no 5 pp 690ndash715 2009

[10] M Bitaraf and S Hurlebaus ldquoSemi-active adaptive control ofseismically excited 20-story nonlinear buildingrdquo EngineeringStructures vol 56 no 11 pp 2107ndash2118 2013

[11] D Das T K Datta and A Madan ldquoSemiactive fuzzy controlof the seismic response of building frames with MR dampersrdquoEarthquake Engineering and Structural Dynamics vol 41 no 1pp 99ndash118 2012

[12] A-P Wang and C-D Lee ldquoFuzzy sliding mode control for abuilding structure based on genetic algorithmsrdquo EarthquakeEngineering and Structural Dynamics vol 31 no 4 pp 881ndash8952002

[13] D G Reigles and M D Symans ldquoSupervisory fuzzy controlof a base-isolated benchmark building utilizing a neuro-fuzzymodel of controllable fluid viscous dampersrdquo Structural Controland Health Monitoring vol 13 no 2-3 pp 724ndash747 2006

[14] H-S Kim and P N Roschke ldquoGA-fuzzy control of smartbase isolated benchmark building using supervisory controltechniquerdquo Advances in Engineering Software vol 38 no 7 pp453ndash465 2007

[15] D Yang and Y Zhao ldquoEffects of rupture forward directivity andfling step of near-fault groundmotions on seismic performanceof base-isolated building structurerdquo Acta Seismologica Sinicavol 32 no 5 pp 579ndash587 2010

[16] Y E-A Mohamedzein J A Abdalla and A Abdelwahab ldquoSiteresponse and earthquake design spectra for central KhartoumSudanrdquoBulletin of Earthquake Engineering vol 4 no 3 pp 277ndash293 2006

[17] D Zhao and H Li ldquoShaking table tests and analyses of semi-active fuzzy control for structural seismic reduction with apiezoelectric variable-friction damperrdquo Smart Materials andStructures vol 19 no 10 Article ID 105031 2010

[18] W L He A K Agrawal and J N Yang ldquoNovel semiactivefriction controller for linear structures against earthquakesrdquoJournal of Structural Engineering vol 129 no 7 pp 941ndash9502003

[19] J N Yang and A K Agrawal ldquoSemi-active hybrid controlsystems for nonlinear buildings against near-field earthquakesrdquoEngineering Structures vol 24 no 3 pp 271ndash280 2002

[20] O E Ozbulut and S Hurlebaus ldquoOptimal design of supere-lastic-friction base isolators for seismic protection of highwaybridges against near-field earthquakesrdquo Earthquake Engineeringand Structural Dynamics vol 40 no 3 pp 273ndash291 2011

[21] D A Shook P N Roschke and O E Ozbulut ldquoSuperelasticsemi-active damping of a base-isolated structurerdquo StructuralControl and HealthMonitoring vol 15 no 5 pp 746ndash768 2008

[22] K D PhamG JinM K Sain B F Spencer Jr and S R LibertyldquoGeneralized linear quadratic Gaussian techniques for the windbenchmark problemrdquo Journal of Engineering Mechanics vol130 no 4 pp 466ndash470 2004

[23] S Nagarajaiah and S Narasimhan ldquoSmart base-isolated bench-mark building Part II Phase I sample controllers for linearisolation systemsrdquo Structural Control and Health Monitoringvol 13 no 2-3 pp 605ndash625 2006

Submit your manuscripts athttpwwwhindawicom

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

MathematicsJournal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Mathematical Problems in Engineering

Hindawi Publishing Corporationhttpwwwhindawicom

Differential EquationsInternational Journal of

Volume 2014

Applied MathematicsJournal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Probability and StatisticsHindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Journal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Mathematical PhysicsAdvances in

Complex AnalysisJournal of

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OptimizationJournal of

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CombinatoricsHindawi Publishing Corporationhttpwwwhindawicom Volume 2014

International Journal of

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Operations ResearchAdvances in

Journal of

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Function Spaces

Abstract and Applied AnalysisHindawi Publishing Corporationhttpwwwhindawicom Volume 2014

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Algebra

Discrete Dynamics in Nature and Society

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

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Decision SciencesAdvances in

Discrete MathematicsJournal of

Hindawi Publishing Corporationhttpwwwhindawicom

Volume 2014 Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Stochastic AnalysisInternational Journal of

Mathematical Problems in Engineering 9

0

1

X

0

1

Deg

ree o

f mem

bers

hip

Deg

ree o

f mem

bers

hip

0

1

Deg

ree o

f mem

bers

hip

1205901

1205901 1205902 1205903

Rule 1 (1 6) Rule 1 (7 12) Rule 5 (24 30)middot middot middot

c1

c1 c2 c3

1205902

Y1

1205903

Y2c2 c3

Figure 10 Encoding structure for genetic algorithm

of piezoelectric friction damper The initial population sizegenetic algebra and crossover probability are set to 20 50and 08 respectively Through inputting the artificial earth-quakes which are characterized by near-fault earthquakesfor different ground sites the supervisory fuzzy control andpreload of piezoelectric friction dampers can be optimizedThe fuzzy control surfaces of optimized supervisory fuzzycontrol are shown in Figure 12

5 Linear Quadratic Gaussian Controller

LQG (Linear Quadratic Gaussian) method is based onKalman filter technique which has become a widely usedcontrol algorithm For comparison purpose LQG is adoptedto regulate the contact normal force of piezoelectric frictiondamper in the study The optimal controller takes groundacceleration as white noise and considers the velocity anddisplacement of base isolation as feedback signals Thecontrol performance index is defined as follows [22]

119869 = lim120591rarr+infin

1

120591

sdot 119864 int

120591

0

[Z (119905)119879QZ (119905) + U (119905)119879RU (119905)] 119889 (119905) (10)

where Q2119899times2119899

and R1times1

are semi-positive definite matrix andpositive definite matrix respectivelyThe control force can beobtained as follows

U (119905) = minusGZ (119905) (11)

G = Rminus1B119879P (12)

where P can be computed by the solution of the Riccatiequation as follows

minusPA minus A119879P + PBRminus1B119879P minusQ = 0 (13)

The control force obtained from the above equation isactive control force which could not be always achieved bypiezoelectric friction damper It is realized that the directionof active control force is opposite to the slipping direction ofpiezoelectric friction damper Therefore the desired controlforce119906

119889(119905) can be achieved according to the following criteria

119906119889(119905)

=

119891max sgn (119887) (119906active

119887lt 0

10038161003816100381610038161003816119906active10038161003816100381610038161003816 gt 119891max)

10038161003816100381610038161003816119906active10038161003816100381610038161003816 sgn (119887) (119906

active119887lt 0

10038161003816100381610038161003816119906active10038161003816100381610038161003816 le 119891max)

119891min sgn (119887) (119906active

119887ge 0)

(14)

10 Mathematical Problems in Engineering

Table 5 Parameters of base-isolated structure

Floor masses(kg)

Stiffness values(kNm)

Dampingcoefficients(kN sm)

Isolated floor 6800 232 745First floor 5897 33732 67Second floor 5897 29093 58Third floor 5897 28621 57Fourth floor 5897 24954 50Fifth floor 5897 19059 38

No

Yes

Encode

Generate initial random population

Calculate the value of fitness and rank

Copy crossover and mutation

Decode

Optimal solution

Whether or not to meet thecondition of convergence

Figure 11 Flow chart of genetic algorithm

where 119906active is the control force obtained from LQG con-troller

119887is the velocity of base isolator119891max and119891min are the

maximum and minimum friction forces of the piezoelectricfriction damper respectively

6 Numerical Simulations

61 Model of the Base-Isolated Structure A five-story base-isolated building which is proposed by He et al is employedto evaluate the performance of developed fuzzy controllers[18] The fundamental period of the five-story building is03 s For the given isolation parameters the fundamentalperiod of the base-isolated building becomes 25 sThereforean isolation ratio 120575 equal to 83 (=2503) is obtainedThe model of the base-isolated structure with piezoelectricfriction damper is shown in Figure 13 The parameters of thebase-isolated structure are shown in Table 5

62 Performance Evaluation Index In order to evaluate theperformance of base-isolated structure for different controlalgorithms a total of nine performance indexes are employedin this study [23] as shown in Table 6

The performance indexes J1through J

5denote the struc-

ture responses for the controlled building normalized byuncontrolled structure respectively The performance indexJ6evaluates the peak control force normalized by the peak

base shear for controlled structure The performance indexesJ7and J8represent RMS (Root Mean Square) base displace-

ments and RMS floor accelerations respectively J9computes

the energy dissipated by friction dampers normalized by theearthquake input energy to the controlled structure

63 Simulation Results and Analysis A total of nine seis-mic excitations that contain six real ground motions andthree artificial earthquakes are selected to evaluate the per-formance of the optimized fuzzy logic controller In thisstudy the time histories of strong earthquake which rangefrom 20 s to 70 s are selected for numerical simulation andanalysis

The numerical results for various earthquakes are listedin Table 7 In the table the Genetic Algorithm HierarchicFuzzy Logic Control is named as GHFLC Moreover forcomparison purpose the results for an optimal controller andpassive operation of friction damper are also listed in thetable Numbers in bold font indicate the best results amongall control cases

Base displacement is an important index to evaluatethe effectiveness for different controllers For a base-isolatedstructure the reduction of base displacement is a primarypurpose to prevent permanent damage for isolation bearingsor adjacent buildings Although passive operation of frictiondampers can successfully reduce the performance indexassociated with the peak and RMS base displacements (J

3and

J7) it causes significant amplification in peak and RMS floor

accelerations (J5and J

8) for most cases due to the passive

control For example as compared to the uncontrolledstructure for TCU052 TCU053 and TCU054 earthquakespassive control leads to 6 45 and 42 amplification inpeak floor acceleration respectively However the proposedfuzzy controller can successfully improve the base-isolatedstructure acceleration at the cost of slight deterioration in theperformance indices J

3and J7on comparison with passive

control For example for TCU052 TCU053 and TCU054earthquakes GHFLC results in 15 13 and 16 decrease inpeak floor accelerations respectively As compared to passivecontrol there are 9 3 and 7 increase in peak basedisplacements

The time histories of friction force and force-displacement curves of friction dampers for differentcontrollers subjected to TCU052 earthquake are shown inFigure 14 From the figures it can be seen that the passivecontrol outputs lager damper force than GHFLC Becausethe supervisory fuzzy control can alter input normalizationfactors of sublevel FLC according to the current level ofground motion there are some serrations presented at theedge of the hysteretic curve of piezoelectric friction damper

The comparison of the performance indexes J3 J7 J5and

J8under different control cases is shown in Figures 15 and

16 respectively From these figures it can be seen that thefuzzy controller is more effective than passive and optimal

Mathematical Problems in Engineering 11O

utpu

t

009

055

026

000033

000094000

Input ground velocity (ms)

Nd

N

(a) Hard soilO

utpu

t

Input ground velocity (ms)

071

042

000

008000

037

103000

Nd

N

(b) Medium soil

Out

put

Input ground velocity (ms)

107

053

000045

011000

117000

Nd

N

(c) Soft soil

Figure 12 Control surface for optimized supervisory fuzzy control

PFD

Fixed reference

LRB

Figure 13 Model of the base-isolated structure

12 Mathematical Problems in Engineering

Table 6 Performance index

Peak base shear Peak interstory drift RMS base displacement

1198691=max119905

10038171003817100381710038171198810 (119905)1003817100381710038171003817

max119905

100381710038171003817100381710038171198810(119905)10038171003817100381710038171003817

1198694=

max119905119891

10038171003817100381710038171003817119889119891(119905)10038171003817100381710038171003817

max119905119891

10038171003817100381710038171003817119889119891(119905)10038171003817100381710038171003817

1198697=

max119894

1003817100381710038171003817120590119889 (119905)1003817100381710038171003817

max119905

1003817100381710038171003817119889 (119905)1003817100381710038171003817

Peak structural shear Peak floor acceleration RMS floor acceleration

1198692=max119905

10038171003817100381710038171198811 (119905)1003817100381710038171003817

max119905

100381710038171003817100381710038171198811(119905)10038171003817100381710038171003817

1198695=

max119905119891

10038171003817100381710038171003817119886119891(119905)10038171003817100381710038171003817

max119905119891

10038171003817100381710038171003817119886119891(119905)10038171003817100381710038171003817

1198698=max119891

1003817100381710038171003817120590119886 (119905)1003817100381710038171003817

max119891

1003817100381710038171003817119886 (119905)1003817100381710038171003817

Peak base displacement Peak control force Energy dissipated by PFD

1198693=max119905

1003817100381710038171003817119909119887 (119905)1003817100381710038171003817

max119905

1003817100381710038171003817119909119887 (119905)1003817100381710038171003817

1198696=max119905

1003817100381710038171003817119891119889 (119905)1003817100381710038171003817

max119905

10038171003817100381710038171198810 (119905)1003817100381710038171003817

1198699=

int119879

0

119891119889(119905) 119887(119905) 119889119905

int119879

0

1198810(119905) 119892(119905) 119889119905

Table 7 Results of numerical simulation

Earthquake Control case 1198691

1198692

1198693

1198694

1198695

1198696

1198697

1198698

1198699

TCU102(hard site)

Passive 081 082 068 085 094 048 057 082 078Optimal 092 095 075 099 087 043 068 081 069GHFLC 087 091 071 093 082 041 061 078 073

TCU052(hard site)

Passive 079 079 046 082 106 036 038 089 087Optimal 087 087 057 087 098 029 049 085 079GHFLC 083 082 055 082 091 033 044 079 084

Artificialearthquake(hard site)

Passive 072 074 054 076 092 054 049 090 084Optimal 084 086 069 083 089 047 057 086 073GHFLC 076 077 061 079 083 042 052 081 076

TCU053(medium site)

Passive 061 065 039 071 145 032 037 116 089Optimal 069 072 046 076 136 031 045 117 078GHFLC 062 062 042 065 132 026 044 109 072

TCU054(medium site)

Passive 071 073 043 073 142 084 038 121 088Optimal 081 087 045 085 132 079 052 125 086GHFLC 075 071 040 074 126 082 045 113 076

Artificialearthquake(medium site)

Passive 054 057 038 064 123 067 036 117 091Optimal 067 066 047 067 119 078 048 113 079GHFLC 058 061 040 062 113 072 041 109 085

TCU110(soft soil site)

Passive 077 078 047 077 103 050 045 089 095Optimal 083 082 052 085 107 046 052 099 087GHFLC 086 086 056 086 104 042 049 093 090

CHY101(soft soil site)

Passive 069 071 058 075 086 066 054 092 084Optimal 075 073 062 074 087 064 055 088 079GHFLC 063 067 054 067 079 065 051 087 083

Artificialearthquake(soft site)

Passive 057 064 061 068 097 061 058 098 088Optimal 071 070 074 075 094 058 071 093 083GHFLC 065 062 067 069 085 055 063 086 076

controller in simultaneously depressing the superstructureacceleration and base displacement For example the appli-cation of developed fuzzy controller leads to an average of112 decrease in peak floor acceleration and an average ofonly 36 increase in peak base displacement as compared topassive control Particularly optimal controller produces anaverage of only 41 reduction in peak floor acceleration and

leads to 79 increase in peak base displacement as comparedto passive control Therefore the improved fuzzy controlmethod shows better performance than passive and optimalcontrol

In order to further evaluate the performance of differentcontrollers the energy time histories for different controllersare compared with each other For a base-isolated structure

Mathematical Problems in Engineering 13

20 30 40 50 60 70minus20

minus10

00

10

20Fr

ictio

n fo

rce (

kN)

Time (s)minus03 minus02 minus01 00 01 02 03

minus20

minus10

00

10

20

Fric

tion

forc

e (kN

)

Displacement (m)

(a) Passive control

20 30 40 50 60 70minus20

minus10

00

10

20

Fric

tion

forc

e (kN

)

Time (s)minus03 minus02 minus01 00 01 02 03

minus20

minus10

00

10

20

Fric

tion

forc

e (kN

)

Displacement (m)

(b) GHFLC method

Figure 14 Time histories of friction force and force-displacement diagram against TCU052 earthquake

1 2 3 4 5 6 7 8 903

04

05

06

07

08

Excitation case

Passive OptimalGHFLC

1 2 3 4 5 6 7 8 903

04

05

06

07

Excitation casePassive

GHFLC Optimal

J 3 J 5

Figure 15 Comparisons on the performance indexes J3and J7for different control cases

14 Mathematical Problems in Engineering

1 2 3 4 5 6 7 8 907

08

09

10

11

12

13

14

15

Excitation casePassive

GHFLC Optimal

1 2 3 4 5 6 7 8 907

08

09

10

11

12

13

Excitation case

Passive

GHFLC Optimal

J 8J 5

Figure 16 Comparison of the performance indexes J5and J8for different control cases

with piezoelectric friction dampers installed on the isolationthe energy equations are defined as follows

119864119870+ 119864120585+ 119864119878+ 119864119867= 119864119868

119864119870=1

2119879

119905119872119905

119864120585= int

119905

0

119879

119888 119889119905

119864119878= int

119905

0

119909119879

119870119889119909

119864119867= minusint

119905

0

119906119879

119864119879

119904119889119909

119864119868= minusint

119905

0

gMI 119889119909

(15)

where 119864119870 119864120585 119864119878 119864119867 and 119864

119868denote the absolute kinetic

energy damping energy elastic strain energy energy dis-sipated by piezoelectric friction dampers and total inputenergy respectively The energy time histories for differentcontrollers against TCU052Chi-Chi earthquake are shown inFigure 17 It can be seen from the figures that the piezoelectricfriction dampers dissipate most of the input energy fordifferent control cases subjected to TCU052 earthquake

In order to compare different effects under near-faultground motions recorded for different sites the average ofinput energy and structure responses subjected to near-faultearthquakes are given in Table 8

As shown in Table 8 the near-fault earthquakes forsoft sites are more destructive than hard sites For instancecompared to hard sites the input energy and the base dis-placement of RMS of the base-isolated structure for soft soil

increase by 143 and 256 respectively However GHFLCpossesses favorable performance under different ground sitesand the damping effect has no distinctly direct relationshipwith site category

As discussed in Section 61 the isolation ratio of thesimulation model equals 83 In order to evaluate the effectsof isolation ratio on the damping performance of GHFLC thestiffness value of isolation is adjusted to 1045 and 452 kNmrespectively Then the numerical results for different valuesof isolation ratio (120575 = 4 6) are obtained The performanceindexes J

3and J5for different isolation ratios are shown in

Figures 18 and 19 respectivelyFor base-isolated structure isolation ratio has a signifi-

cant influence on the isolation effect A larger isolation ratiowhich means a minor stiffness value of isolation usuallyleads to conspicuous enlargement of base displacement anddecrease of superstructural responses due to the increaseof fundamental vibration period and vice versa Howeveras shown in Figures 18 and 19 the shock absorption rateof GHFLC has little change when isolation ratio variesdifferently and the proposed fuzzy control shows favorableeffectiveness in the diverse isolation ratios of base-isolatedstructures

7 Conclusions

In this study an optimized fuzzy logic control which isdesigned for Chi-Chi near-fault earthquakes under differentground sites is proposed An elastic design spectrum isproposed to generate near-fault earthquakes for differentground sitesThe characteristic of the design spectrum is thatit has larger periods and peak acceleration than conventionalspectrum Genetic algorithm is employed to optimize thesupervisory fuzzy controller and preload of piezoelectric

Mathematical Problems in Engineering 15

Table 8 Average ofinput energy and structure responses subjected to near-fault earthquakes

Site classification Input energy (kNsdotm) Base shear (kN) Base displacement ofRMS (m)

Structure accelerationof RMS (g)

Hard soil 24375 475 0047 0432Medium soil 26746 498 0054 0476Soft soil 27857 568 0059 0531

20 30 40 50 60 7000

05

10

15

20

25

Input energyEnergy dissipated by dampers

Time (s)

Ener

gy (k

Nmiddotm

)

times104

(a) Passive control

20 30 40 50 60 7000

05

10

15

20

25

30

Time (s)

Input energyEnergy dissipated by dampers

Ener

gy (k

Nmiddotm

)

times104

(b) Optimal control

20 30 40 50 60 7000

05

10

15

20

25

30

Input energyEnergy dissipated by dampers

Time (s)

Ener

gy (k

Nmiddotm

)

times104

(c) GHFLC method

Figure 17 Energy time histories subjected to Chi-Chi TCU052 earthquake

friction dampers according to three artificial earthquakesthat are characterized by Chi-Chi earthquakes Passive andoptimal controllers are also compared with the performanceof the developed fuzzy controller The simulation resultsreveal that the developed semiactive fuzzy controller hasbetter performance than traditional passive and optimal con-troller in simultaneously reducing the base displacement and

floor acceleration under near-fault earthquakes for differentground sites

Conflict of Interests

The authors declare no conflict of interests regarding thepublication of this paper

16 Mathematical Problems in Engineering

1 2 3 4 5 6 7 8 903

04

05

06

07

08

Excitation casePassive

GHFLC Optimal

1 2 3 4 5 6 7 8 907

08

09

10

11

12

13

14

15

Excitation case

Passive

GHFLC Optimal

J 3 J 5Figure 18 Comparisons on the performance indexes J

3and J5for different control cases (120575 = 4)

1 2 3 4 5 6 7 8 903

04

05

06

07

08

Excitation casePassive

GHFLC Optimal

1 2 3 4 5 6 7 8 907

08

09

10

11

12

13

14

15

Excitation casePassive

GHFLC Optimal

J 3 J 5

Figure 19 Comparisons on the performance indexes J3and J5for different control cases (120575 = 6)

Acknowledgments

This research was supported by National Natural ScienceFoundation of China under Grant no 51308487 no 41402261and no 51408526 Hebei Provincial Natural Science Founda-tion ofChina underGrant no E2014203055 and the ExcellentYouth Foundation of Hebei Educational Committee underGrant no YQ2013015 The support for this research is greatlyappreciated

References

[1] C Alhan and H Gavin ldquoA parametric study of linear and non-linear passively damped seismic isolation systems for buildingsrdquoEngineering Structures vol 26 no 4 pp 485ndash497 2004

[2] R S Jangid and J M Kelly ldquoBase isolation for near-faultmotionsrdquoEarthquake Engineering and Structural Dynamics vol30 no 5 pp 691ndash707 2001

[3] J Shen M-H Tsai K-C Chang and G C Lee ldquoPerformanceof a seismically isolated bridge under near-fault earthquake

Mathematical Problems in Engineering 17

ground motionsrdquo Journal of Structural Engineering vol 130 no6 pp 861ndash868 2004

[4] F Mazza A Vulcano and M Mazza ldquoNonlinear dynamicresponse of RC buildings with different base Isolation systemssubjected to horizontal and vertical components of near-faultground motionsrdquo Open Construction and Building TechnologyJournal vol 6 pp 373ndash383 2012

[5] F Mazza and A Vulcano ldquoEffects of near-fault ground motionson the nonlinear dynamic response of base-isolated rc framedbuildingsrdquo Earthquake Engineering and Structural Dynamicsvol 41 no 2 pp 211ndash232 2012

[6] O E Ozbulut and S Hurlebaus ldquoFuzzy control of piezoelectricfriction dampers for seismic protection of smart base isolatedbuildingsrdquo Bulletin of Earthquake Engineering vol 8 no 6 pp1435ndash1455 2010

[7] O E Ozbulut M Bitaraf and S Hurlebaus ldquoAdaptive controlof base-isolated structures against near-field earthquakes usingvariable friction dampersrdquo Engineering Structures vol 33 no12 pp 3143ndash3154 2011

[8] J M Kelly ldquoThe role of damping in seismic isolationrdquo Earth-quake Engineering and Structural Dynamics vol 28 no 1 pp3ndash20 1999

[9] F Mazza and A Vulcano ldquoNonlinear response of RC framedbuildings with isolation and supplemental damping at the basesubjected to near-fault earthquakesrdquo Journal of EarthquakeEngineering vol 13 no 5 pp 690ndash715 2009

[10] M Bitaraf and S Hurlebaus ldquoSemi-active adaptive control ofseismically excited 20-story nonlinear buildingrdquo EngineeringStructures vol 56 no 11 pp 2107ndash2118 2013

[11] D Das T K Datta and A Madan ldquoSemiactive fuzzy controlof the seismic response of building frames with MR dampersrdquoEarthquake Engineering and Structural Dynamics vol 41 no 1pp 99ndash118 2012

[12] A-P Wang and C-D Lee ldquoFuzzy sliding mode control for abuilding structure based on genetic algorithmsrdquo EarthquakeEngineering and Structural Dynamics vol 31 no 4 pp 881ndash8952002

[13] D G Reigles and M D Symans ldquoSupervisory fuzzy controlof a base-isolated benchmark building utilizing a neuro-fuzzymodel of controllable fluid viscous dampersrdquo Structural Controland Health Monitoring vol 13 no 2-3 pp 724ndash747 2006

[14] H-S Kim and P N Roschke ldquoGA-fuzzy control of smartbase isolated benchmark building using supervisory controltechniquerdquo Advances in Engineering Software vol 38 no 7 pp453ndash465 2007

[15] D Yang and Y Zhao ldquoEffects of rupture forward directivity andfling step of near-fault groundmotions on seismic performanceof base-isolated building structurerdquo Acta Seismologica Sinicavol 32 no 5 pp 579ndash587 2010

[16] Y E-A Mohamedzein J A Abdalla and A Abdelwahab ldquoSiteresponse and earthquake design spectra for central KhartoumSudanrdquoBulletin of Earthquake Engineering vol 4 no 3 pp 277ndash293 2006

[17] D Zhao and H Li ldquoShaking table tests and analyses of semi-active fuzzy control for structural seismic reduction with apiezoelectric variable-friction damperrdquo Smart Materials andStructures vol 19 no 10 Article ID 105031 2010

[18] W L He A K Agrawal and J N Yang ldquoNovel semiactivefriction controller for linear structures against earthquakesrdquoJournal of Structural Engineering vol 129 no 7 pp 941ndash9502003

[19] J N Yang and A K Agrawal ldquoSemi-active hybrid controlsystems for nonlinear buildings against near-field earthquakesrdquoEngineering Structures vol 24 no 3 pp 271ndash280 2002

[20] O E Ozbulut and S Hurlebaus ldquoOptimal design of supere-lastic-friction base isolators for seismic protection of highwaybridges against near-field earthquakesrdquo Earthquake Engineeringand Structural Dynamics vol 40 no 3 pp 273ndash291 2011

[21] D A Shook P N Roschke and O E Ozbulut ldquoSuperelasticsemi-active damping of a base-isolated structurerdquo StructuralControl and HealthMonitoring vol 15 no 5 pp 746ndash768 2008

[22] K D PhamG JinM K Sain B F Spencer Jr and S R LibertyldquoGeneralized linear quadratic Gaussian techniques for the windbenchmark problemrdquo Journal of Engineering Mechanics vol130 no 4 pp 466ndash470 2004

[23] S Nagarajaiah and S Narasimhan ldquoSmart base-isolated bench-mark building Part II Phase I sample controllers for linearisolation systemsrdquo Structural Control and Health Monitoringvol 13 no 2-3 pp 605ndash625 2006

Submit your manuscripts athttpwwwhindawicom

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

MathematicsJournal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Mathematical Problems in Engineering

Hindawi Publishing Corporationhttpwwwhindawicom

Differential EquationsInternational Journal of

Volume 2014

Applied MathematicsJournal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Probability and StatisticsHindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Journal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Mathematical PhysicsAdvances in

Complex AnalysisJournal of

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OptimizationJournal of

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CombinatoricsHindawi Publishing Corporationhttpwwwhindawicom Volume 2014

International Journal of

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Operations ResearchAdvances in

Journal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Function Spaces

Abstract and Applied AnalysisHindawi Publishing Corporationhttpwwwhindawicom Volume 2014

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Algebra

Discrete Dynamics in Nature and Society

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Decision SciencesAdvances in

Discrete MathematicsJournal of

Hindawi Publishing Corporationhttpwwwhindawicom

Volume 2014 Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Stochastic AnalysisInternational Journal of

10 Mathematical Problems in Engineering

Table 5 Parameters of base-isolated structure

Floor masses(kg)

Stiffness values(kNm)

Dampingcoefficients(kN sm)

Isolated floor 6800 232 745First floor 5897 33732 67Second floor 5897 29093 58Third floor 5897 28621 57Fourth floor 5897 24954 50Fifth floor 5897 19059 38

No

Yes

Encode

Generate initial random population

Calculate the value of fitness and rank

Copy crossover and mutation

Decode

Optimal solution

Whether or not to meet thecondition of convergence

Figure 11 Flow chart of genetic algorithm

where 119906active is the control force obtained from LQG con-troller

119887is the velocity of base isolator119891max and119891min are the

maximum and minimum friction forces of the piezoelectricfriction damper respectively

6 Numerical Simulations

61 Model of the Base-Isolated Structure A five-story base-isolated building which is proposed by He et al is employedto evaluate the performance of developed fuzzy controllers[18] The fundamental period of the five-story building is03 s For the given isolation parameters the fundamentalperiod of the base-isolated building becomes 25 sThereforean isolation ratio 120575 equal to 83 (=2503) is obtainedThe model of the base-isolated structure with piezoelectricfriction damper is shown in Figure 13 The parameters of thebase-isolated structure are shown in Table 5

62 Performance Evaluation Index In order to evaluate theperformance of base-isolated structure for different controlalgorithms a total of nine performance indexes are employedin this study [23] as shown in Table 6

The performance indexes J1through J

5denote the struc-

ture responses for the controlled building normalized byuncontrolled structure respectively The performance indexJ6evaluates the peak control force normalized by the peak

base shear for controlled structure The performance indexesJ7and J8represent RMS (Root Mean Square) base displace-

ments and RMS floor accelerations respectively J9computes

the energy dissipated by friction dampers normalized by theearthquake input energy to the controlled structure

63 Simulation Results and Analysis A total of nine seis-mic excitations that contain six real ground motions andthree artificial earthquakes are selected to evaluate the per-formance of the optimized fuzzy logic controller In thisstudy the time histories of strong earthquake which rangefrom 20 s to 70 s are selected for numerical simulation andanalysis

The numerical results for various earthquakes are listedin Table 7 In the table the Genetic Algorithm HierarchicFuzzy Logic Control is named as GHFLC Moreover forcomparison purpose the results for an optimal controller andpassive operation of friction damper are also listed in thetable Numbers in bold font indicate the best results amongall control cases

Base displacement is an important index to evaluatethe effectiveness for different controllers For a base-isolatedstructure the reduction of base displacement is a primarypurpose to prevent permanent damage for isolation bearingsor adjacent buildings Although passive operation of frictiondampers can successfully reduce the performance indexassociated with the peak and RMS base displacements (J

3and

J7) it causes significant amplification in peak and RMS floor

accelerations (J5and J

8) for most cases due to the passive

control For example as compared to the uncontrolledstructure for TCU052 TCU053 and TCU054 earthquakespassive control leads to 6 45 and 42 amplification inpeak floor acceleration respectively However the proposedfuzzy controller can successfully improve the base-isolatedstructure acceleration at the cost of slight deterioration in theperformance indices J

3and J7on comparison with passive

control For example for TCU052 TCU053 and TCU054earthquakes GHFLC results in 15 13 and 16 decrease inpeak floor accelerations respectively As compared to passivecontrol there are 9 3 and 7 increase in peak basedisplacements

The time histories of friction force and force-displacement curves of friction dampers for differentcontrollers subjected to TCU052 earthquake are shown inFigure 14 From the figures it can be seen that the passivecontrol outputs lager damper force than GHFLC Becausethe supervisory fuzzy control can alter input normalizationfactors of sublevel FLC according to the current level ofground motion there are some serrations presented at theedge of the hysteretic curve of piezoelectric friction damper

The comparison of the performance indexes J3 J7 J5and

J8under different control cases is shown in Figures 15 and

16 respectively From these figures it can be seen that thefuzzy controller is more effective than passive and optimal

Mathematical Problems in Engineering 11O

utpu

t

009

055

026

000033

000094000

Input ground velocity (ms)

Nd

N

(a) Hard soilO

utpu

t

Input ground velocity (ms)

071

042

000

008000

037

103000

Nd

N

(b) Medium soil

Out

put

Input ground velocity (ms)

107

053

000045

011000

117000

Nd

N

(c) Soft soil

Figure 12 Control surface for optimized supervisory fuzzy control

PFD

Fixed reference

LRB

Figure 13 Model of the base-isolated structure

12 Mathematical Problems in Engineering

Table 6 Performance index

Peak base shear Peak interstory drift RMS base displacement

1198691=max119905

10038171003817100381710038171198810 (119905)1003817100381710038171003817

max119905

100381710038171003817100381710038171198810(119905)10038171003817100381710038171003817

1198694=

max119905119891

10038171003817100381710038171003817119889119891(119905)10038171003817100381710038171003817

max119905119891

10038171003817100381710038171003817119889119891(119905)10038171003817100381710038171003817

1198697=

max119894

1003817100381710038171003817120590119889 (119905)1003817100381710038171003817

max119905

1003817100381710038171003817119889 (119905)1003817100381710038171003817

Peak structural shear Peak floor acceleration RMS floor acceleration

1198692=max119905

10038171003817100381710038171198811 (119905)1003817100381710038171003817

max119905

100381710038171003817100381710038171198811(119905)10038171003817100381710038171003817

1198695=

max119905119891

10038171003817100381710038171003817119886119891(119905)10038171003817100381710038171003817

max119905119891

10038171003817100381710038171003817119886119891(119905)10038171003817100381710038171003817

1198698=max119891

1003817100381710038171003817120590119886 (119905)1003817100381710038171003817

max119891

1003817100381710038171003817119886 (119905)1003817100381710038171003817

Peak base displacement Peak control force Energy dissipated by PFD

1198693=max119905

1003817100381710038171003817119909119887 (119905)1003817100381710038171003817

max119905

1003817100381710038171003817119909119887 (119905)1003817100381710038171003817

1198696=max119905

1003817100381710038171003817119891119889 (119905)1003817100381710038171003817

max119905

10038171003817100381710038171198810 (119905)1003817100381710038171003817

1198699=

int119879

0

119891119889(119905) 119887(119905) 119889119905

int119879

0

1198810(119905) 119892(119905) 119889119905

Table 7 Results of numerical simulation

Earthquake Control case 1198691

1198692

1198693

1198694

1198695

1198696

1198697

1198698

1198699

TCU102(hard site)

Passive 081 082 068 085 094 048 057 082 078Optimal 092 095 075 099 087 043 068 081 069GHFLC 087 091 071 093 082 041 061 078 073

TCU052(hard site)

Passive 079 079 046 082 106 036 038 089 087Optimal 087 087 057 087 098 029 049 085 079GHFLC 083 082 055 082 091 033 044 079 084

Artificialearthquake(hard site)

Passive 072 074 054 076 092 054 049 090 084Optimal 084 086 069 083 089 047 057 086 073GHFLC 076 077 061 079 083 042 052 081 076

TCU053(medium site)

Passive 061 065 039 071 145 032 037 116 089Optimal 069 072 046 076 136 031 045 117 078GHFLC 062 062 042 065 132 026 044 109 072

TCU054(medium site)

Passive 071 073 043 073 142 084 038 121 088Optimal 081 087 045 085 132 079 052 125 086GHFLC 075 071 040 074 126 082 045 113 076

Artificialearthquake(medium site)

Passive 054 057 038 064 123 067 036 117 091Optimal 067 066 047 067 119 078 048 113 079GHFLC 058 061 040 062 113 072 041 109 085

TCU110(soft soil site)

Passive 077 078 047 077 103 050 045 089 095Optimal 083 082 052 085 107 046 052 099 087GHFLC 086 086 056 086 104 042 049 093 090

CHY101(soft soil site)

Passive 069 071 058 075 086 066 054 092 084Optimal 075 073 062 074 087 064 055 088 079GHFLC 063 067 054 067 079 065 051 087 083

Artificialearthquake(soft site)

Passive 057 064 061 068 097 061 058 098 088Optimal 071 070 074 075 094 058 071 093 083GHFLC 065 062 067 069 085 055 063 086 076

controller in simultaneously depressing the superstructureacceleration and base displacement For example the appli-cation of developed fuzzy controller leads to an average of112 decrease in peak floor acceleration and an average ofonly 36 increase in peak base displacement as compared topassive control Particularly optimal controller produces anaverage of only 41 reduction in peak floor acceleration and

leads to 79 increase in peak base displacement as comparedto passive control Therefore the improved fuzzy controlmethod shows better performance than passive and optimalcontrol

In order to further evaluate the performance of differentcontrollers the energy time histories for different controllersare compared with each other For a base-isolated structure

Mathematical Problems in Engineering 13

20 30 40 50 60 70minus20

minus10

00

10

20Fr

ictio

n fo

rce (

kN)

Time (s)minus03 minus02 minus01 00 01 02 03

minus20

minus10

00

10

20

Fric

tion

forc

e (kN

)

Displacement (m)

(a) Passive control

20 30 40 50 60 70minus20

minus10

00

10

20

Fric

tion

forc

e (kN

)

Time (s)minus03 minus02 minus01 00 01 02 03

minus20

minus10

00

10

20

Fric

tion

forc

e (kN

)

Displacement (m)

(b) GHFLC method

Figure 14 Time histories of friction force and force-displacement diagram against TCU052 earthquake

1 2 3 4 5 6 7 8 903

04

05

06

07

08

Excitation case

Passive OptimalGHFLC

1 2 3 4 5 6 7 8 903

04

05

06

07

Excitation casePassive

GHFLC Optimal

J 3 J 5

Figure 15 Comparisons on the performance indexes J3and J7for different control cases

14 Mathematical Problems in Engineering

1 2 3 4 5 6 7 8 907

08

09

10

11

12

13

14

15

Excitation casePassive

GHFLC Optimal

1 2 3 4 5 6 7 8 907

08

09

10

11

12

13

Excitation case

Passive

GHFLC Optimal

J 8J 5

Figure 16 Comparison of the performance indexes J5and J8for different control cases

with piezoelectric friction dampers installed on the isolationthe energy equations are defined as follows

119864119870+ 119864120585+ 119864119878+ 119864119867= 119864119868

119864119870=1

2119879

119905119872119905

119864120585= int

119905

0

119879

119888 119889119905

119864119878= int

119905

0

119909119879

119870119889119909

119864119867= minusint

119905

0

119906119879

119864119879

119904119889119909

119864119868= minusint

119905

0

gMI 119889119909

(15)

where 119864119870 119864120585 119864119878 119864119867 and 119864

119868denote the absolute kinetic

energy damping energy elastic strain energy energy dis-sipated by piezoelectric friction dampers and total inputenergy respectively The energy time histories for differentcontrollers against TCU052Chi-Chi earthquake are shown inFigure 17 It can be seen from the figures that the piezoelectricfriction dampers dissipate most of the input energy fordifferent control cases subjected to TCU052 earthquake

In order to compare different effects under near-faultground motions recorded for different sites the average ofinput energy and structure responses subjected to near-faultearthquakes are given in Table 8

As shown in Table 8 the near-fault earthquakes forsoft sites are more destructive than hard sites For instancecompared to hard sites the input energy and the base dis-placement of RMS of the base-isolated structure for soft soil

increase by 143 and 256 respectively However GHFLCpossesses favorable performance under different ground sitesand the damping effect has no distinctly direct relationshipwith site category

As discussed in Section 61 the isolation ratio of thesimulation model equals 83 In order to evaluate the effectsof isolation ratio on the damping performance of GHFLC thestiffness value of isolation is adjusted to 1045 and 452 kNmrespectively Then the numerical results for different valuesof isolation ratio (120575 = 4 6) are obtained The performanceindexes J

3and J5for different isolation ratios are shown in

Figures 18 and 19 respectivelyFor base-isolated structure isolation ratio has a signifi-

cant influence on the isolation effect A larger isolation ratiowhich means a minor stiffness value of isolation usuallyleads to conspicuous enlargement of base displacement anddecrease of superstructural responses due to the increaseof fundamental vibration period and vice versa Howeveras shown in Figures 18 and 19 the shock absorption rateof GHFLC has little change when isolation ratio variesdifferently and the proposed fuzzy control shows favorableeffectiveness in the diverse isolation ratios of base-isolatedstructures

7 Conclusions

In this study an optimized fuzzy logic control which isdesigned for Chi-Chi near-fault earthquakes under differentground sites is proposed An elastic design spectrum isproposed to generate near-fault earthquakes for differentground sitesThe characteristic of the design spectrum is thatit has larger periods and peak acceleration than conventionalspectrum Genetic algorithm is employed to optimize thesupervisory fuzzy controller and preload of piezoelectric

Mathematical Problems in Engineering 15

Table 8 Average ofinput energy and structure responses subjected to near-fault earthquakes

Site classification Input energy (kNsdotm) Base shear (kN) Base displacement ofRMS (m)

Structure accelerationof RMS (g)

Hard soil 24375 475 0047 0432Medium soil 26746 498 0054 0476Soft soil 27857 568 0059 0531

20 30 40 50 60 7000

05

10

15

20

25

Input energyEnergy dissipated by dampers

Time (s)

Ener

gy (k

Nmiddotm

)

times104

(a) Passive control

20 30 40 50 60 7000

05

10

15

20

25

30

Time (s)

Input energyEnergy dissipated by dampers

Ener

gy (k

Nmiddotm

)

times104

(b) Optimal control

20 30 40 50 60 7000

05

10

15

20

25

30

Input energyEnergy dissipated by dampers

Time (s)

Ener

gy (k

Nmiddotm

)

times104

(c) GHFLC method

Figure 17 Energy time histories subjected to Chi-Chi TCU052 earthquake

friction dampers according to three artificial earthquakesthat are characterized by Chi-Chi earthquakes Passive andoptimal controllers are also compared with the performanceof the developed fuzzy controller The simulation resultsreveal that the developed semiactive fuzzy controller hasbetter performance than traditional passive and optimal con-troller in simultaneously reducing the base displacement and

floor acceleration under near-fault earthquakes for differentground sites

Conflict of Interests

The authors declare no conflict of interests regarding thepublication of this paper

16 Mathematical Problems in Engineering

1 2 3 4 5 6 7 8 903

04

05

06

07

08

Excitation casePassive

GHFLC Optimal

1 2 3 4 5 6 7 8 907

08

09

10

11

12

13

14

15

Excitation case

Passive

GHFLC Optimal

J 3 J 5Figure 18 Comparisons on the performance indexes J

3and J5for different control cases (120575 = 4)

1 2 3 4 5 6 7 8 903

04

05

06

07

08

Excitation casePassive

GHFLC Optimal

1 2 3 4 5 6 7 8 907

08

09

10

11

12

13

14

15

Excitation casePassive

GHFLC Optimal

J 3 J 5

Figure 19 Comparisons on the performance indexes J3and J5for different control cases (120575 = 6)

Acknowledgments

This research was supported by National Natural ScienceFoundation of China under Grant no 51308487 no 41402261and no 51408526 Hebei Provincial Natural Science Founda-tion ofChina underGrant no E2014203055 and the ExcellentYouth Foundation of Hebei Educational Committee underGrant no YQ2013015 The support for this research is greatlyappreciated

References

[1] C Alhan and H Gavin ldquoA parametric study of linear and non-linear passively damped seismic isolation systems for buildingsrdquoEngineering Structures vol 26 no 4 pp 485ndash497 2004

[2] R S Jangid and J M Kelly ldquoBase isolation for near-faultmotionsrdquoEarthquake Engineering and Structural Dynamics vol30 no 5 pp 691ndash707 2001

[3] J Shen M-H Tsai K-C Chang and G C Lee ldquoPerformanceof a seismically isolated bridge under near-fault earthquake

Mathematical Problems in Engineering 17

ground motionsrdquo Journal of Structural Engineering vol 130 no6 pp 861ndash868 2004

[4] F Mazza A Vulcano and M Mazza ldquoNonlinear dynamicresponse of RC buildings with different base Isolation systemssubjected to horizontal and vertical components of near-faultground motionsrdquo Open Construction and Building TechnologyJournal vol 6 pp 373ndash383 2012

[5] F Mazza and A Vulcano ldquoEffects of near-fault ground motionson the nonlinear dynamic response of base-isolated rc framedbuildingsrdquo Earthquake Engineering and Structural Dynamicsvol 41 no 2 pp 211ndash232 2012

[6] O E Ozbulut and S Hurlebaus ldquoFuzzy control of piezoelectricfriction dampers for seismic protection of smart base isolatedbuildingsrdquo Bulletin of Earthquake Engineering vol 8 no 6 pp1435ndash1455 2010

[7] O E Ozbulut M Bitaraf and S Hurlebaus ldquoAdaptive controlof base-isolated structures against near-field earthquakes usingvariable friction dampersrdquo Engineering Structures vol 33 no12 pp 3143ndash3154 2011

[8] J M Kelly ldquoThe role of damping in seismic isolationrdquo Earth-quake Engineering and Structural Dynamics vol 28 no 1 pp3ndash20 1999

[9] F Mazza and A Vulcano ldquoNonlinear response of RC framedbuildings with isolation and supplemental damping at the basesubjected to near-fault earthquakesrdquo Journal of EarthquakeEngineering vol 13 no 5 pp 690ndash715 2009

[10] M Bitaraf and S Hurlebaus ldquoSemi-active adaptive control ofseismically excited 20-story nonlinear buildingrdquo EngineeringStructures vol 56 no 11 pp 2107ndash2118 2013

[11] D Das T K Datta and A Madan ldquoSemiactive fuzzy controlof the seismic response of building frames with MR dampersrdquoEarthquake Engineering and Structural Dynamics vol 41 no 1pp 99ndash118 2012

[12] A-P Wang and C-D Lee ldquoFuzzy sliding mode control for abuilding structure based on genetic algorithmsrdquo EarthquakeEngineering and Structural Dynamics vol 31 no 4 pp 881ndash8952002

[13] D G Reigles and M D Symans ldquoSupervisory fuzzy controlof a base-isolated benchmark building utilizing a neuro-fuzzymodel of controllable fluid viscous dampersrdquo Structural Controland Health Monitoring vol 13 no 2-3 pp 724ndash747 2006

[14] H-S Kim and P N Roschke ldquoGA-fuzzy control of smartbase isolated benchmark building using supervisory controltechniquerdquo Advances in Engineering Software vol 38 no 7 pp453ndash465 2007

[15] D Yang and Y Zhao ldquoEffects of rupture forward directivity andfling step of near-fault groundmotions on seismic performanceof base-isolated building structurerdquo Acta Seismologica Sinicavol 32 no 5 pp 579ndash587 2010

[16] Y E-A Mohamedzein J A Abdalla and A Abdelwahab ldquoSiteresponse and earthquake design spectra for central KhartoumSudanrdquoBulletin of Earthquake Engineering vol 4 no 3 pp 277ndash293 2006

[17] D Zhao and H Li ldquoShaking table tests and analyses of semi-active fuzzy control for structural seismic reduction with apiezoelectric variable-friction damperrdquo Smart Materials andStructures vol 19 no 10 Article ID 105031 2010

[18] W L He A K Agrawal and J N Yang ldquoNovel semiactivefriction controller for linear structures against earthquakesrdquoJournal of Structural Engineering vol 129 no 7 pp 941ndash9502003

[19] J N Yang and A K Agrawal ldquoSemi-active hybrid controlsystems for nonlinear buildings against near-field earthquakesrdquoEngineering Structures vol 24 no 3 pp 271ndash280 2002

[20] O E Ozbulut and S Hurlebaus ldquoOptimal design of supere-lastic-friction base isolators for seismic protection of highwaybridges against near-field earthquakesrdquo Earthquake Engineeringand Structural Dynamics vol 40 no 3 pp 273ndash291 2011

[21] D A Shook P N Roschke and O E Ozbulut ldquoSuperelasticsemi-active damping of a base-isolated structurerdquo StructuralControl and HealthMonitoring vol 15 no 5 pp 746ndash768 2008

[22] K D PhamG JinM K Sain B F Spencer Jr and S R LibertyldquoGeneralized linear quadratic Gaussian techniques for the windbenchmark problemrdquo Journal of Engineering Mechanics vol130 no 4 pp 466ndash470 2004

[23] S Nagarajaiah and S Narasimhan ldquoSmart base-isolated bench-mark building Part II Phase I sample controllers for linearisolation systemsrdquo Structural Control and Health Monitoringvol 13 no 2-3 pp 605ndash625 2006

Submit your manuscripts athttpwwwhindawicom

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

MathematicsJournal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Mathematical Problems in Engineering

Hindawi Publishing Corporationhttpwwwhindawicom

Differential EquationsInternational Journal of

Volume 2014

Applied MathematicsJournal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Probability and StatisticsHindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Journal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Mathematical PhysicsAdvances in

Complex AnalysisJournal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

OptimizationJournal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

CombinatoricsHindawi Publishing Corporationhttpwwwhindawicom Volume 2014

International Journal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Operations ResearchAdvances in

Journal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Function Spaces

Abstract and Applied AnalysisHindawi Publishing Corporationhttpwwwhindawicom Volume 2014

International Journal of Mathematics and Mathematical Sciences

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

The Scientific World JournalHindawi Publishing Corporation httpwwwhindawicom Volume 2014

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Algebra

Discrete Dynamics in Nature and Society

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Decision SciencesAdvances in

Discrete MathematicsJournal of

Hindawi Publishing Corporationhttpwwwhindawicom

Volume 2014 Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Stochastic AnalysisInternational Journal of

Mathematical Problems in Engineering 11O

utpu

t

009

055

026

000033

000094000

Input ground velocity (ms)

Nd

N

(a) Hard soilO

utpu

t

Input ground velocity (ms)

071

042

000

008000

037

103000

Nd

N

(b) Medium soil

Out

put

Input ground velocity (ms)

107

053

000045

011000

117000

Nd

N

(c) Soft soil

Figure 12 Control surface for optimized supervisory fuzzy control

PFD

Fixed reference

LRB

Figure 13 Model of the base-isolated structure

12 Mathematical Problems in Engineering

Table 6 Performance index

Peak base shear Peak interstory drift RMS base displacement

1198691=max119905

10038171003817100381710038171198810 (119905)1003817100381710038171003817

max119905

100381710038171003817100381710038171198810(119905)10038171003817100381710038171003817

1198694=

max119905119891

10038171003817100381710038171003817119889119891(119905)10038171003817100381710038171003817

max119905119891

10038171003817100381710038171003817119889119891(119905)10038171003817100381710038171003817

1198697=

max119894

1003817100381710038171003817120590119889 (119905)1003817100381710038171003817

max119905

1003817100381710038171003817119889 (119905)1003817100381710038171003817

Peak structural shear Peak floor acceleration RMS floor acceleration

1198692=max119905

10038171003817100381710038171198811 (119905)1003817100381710038171003817

max119905

100381710038171003817100381710038171198811(119905)10038171003817100381710038171003817

1198695=

max119905119891

10038171003817100381710038171003817119886119891(119905)10038171003817100381710038171003817

max119905119891

10038171003817100381710038171003817119886119891(119905)10038171003817100381710038171003817

1198698=max119891

1003817100381710038171003817120590119886 (119905)1003817100381710038171003817

max119891

1003817100381710038171003817119886 (119905)1003817100381710038171003817

Peak base displacement Peak control force Energy dissipated by PFD

1198693=max119905

1003817100381710038171003817119909119887 (119905)1003817100381710038171003817

max119905

1003817100381710038171003817119909119887 (119905)1003817100381710038171003817

1198696=max119905

1003817100381710038171003817119891119889 (119905)1003817100381710038171003817

max119905

10038171003817100381710038171198810 (119905)1003817100381710038171003817

1198699=

int119879

0

119891119889(119905) 119887(119905) 119889119905

int119879

0

1198810(119905) 119892(119905) 119889119905

Table 7 Results of numerical simulation

Earthquake Control case 1198691

1198692

1198693

1198694

1198695

1198696

1198697

1198698

1198699

TCU102(hard site)

Passive 081 082 068 085 094 048 057 082 078Optimal 092 095 075 099 087 043 068 081 069GHFLC 087 091 071 093 082 041 061 078 073

TCU052(hard site)

Passive 079 079 046 082 106 036 038 089 087Optimal 087 087 057 087 098 029 049 085 079GHFLC 083 082 055 082 091 033 044 079 084

Artificialearthquake(hard site)

Passive 072 074 054 076 092 054 049 090 084Optimal 084 086 069 083 089 047 057 086 073GHFLC 076 077 061 079 083 042 052 081 076

TCU053(medium site)

Passive 061 065 039 071 145 032 037 116 089Optimal 069 072 046 076 136 031 045 117 078GHFLC 062 062 042 065 132 026 044 109 072

TCU054(medium site)

Passive 071 073 043 073 142 084 038 121 088Optimal 081 087 045 085 132 079 052 125 086GHFLC 075 071 040 074 126 082 045 113 076

Artificialearthquake(medium site)

Passive 054 057 038 064 123 067 036 117 091Optimal 067 066 047 067 119 078 048 113 079GHFLC 058 061 040 062 113 072 041 109 085

TCU110(soft soil site)

Passive 077 078 047 077 103 050 045 089 095Optimal 083 082 052 085 107 046 052 099 087GHFLC 086 086 056 086 104 042 049 093 090

CHY101(soft soil site)

Passive 069 071 058 075 086 066 054 092 084Optimal 075 073 062 074 087 064 055 088 079GHFLC 063 067 054 067 079 065 051 087 083

Artificialearthquake(soft site)

Passive 057 064 061 068 097 061 058 098 088Optimal 071 070 074 075 094 058 071 093 083GHFLC 065 062 067 069 085 055 063 086 076

controller in simultaneously depressing the superstructureacceleration and base displacement For example the appli-cation of developed fuzzy controller leads to an average of112 decrease in peak floor acceleration and an average ofonly 36 increase in peak base displacement as compared topassive control Particularly optimal controller produces anaverage of only 41 reduction in peak floor acceleration and

leads to 79 increase in peak base displacement as comparedto passive control Therefore the improved fuzzy controlmethod shows better performance than passive and optimalcontrol

In order to further evaluate the performance of differentcontrollers the energy time histories for different controllersare compared with each other For a base-isolated structure

Mathematical Problems in Engineering 13

20 30 40 50 60 70minus20

minus10

00

10

20Fr

ictio

n fo

rce (

kN)

Time (s)minus03 minus02 minus01 00 01 02 03

minus20

minus10

00

10

20

Fric

tion

forc

e (kN

)

Displacement (m)

(a) Passive control

20 30 40 50 60 70minus20

minus10

00

10

20

Fric

tion

forc

e (kN

)

Time (s)minus03 minus02 minus01 00 01 02 03

minus20

minus10

00

10

20

Fric

tion

forc

e (kN

)

Displacement (m)

(b) GHFLC method

Figure 14 Time histories of friction force and force-displacement diagram against TCU052 earthquake

1 2 3 4 5 6 7 8 903

04

05

06

07

08

Excitation case

Passive OptimalGHFLC

1 2 3 4 5 6 7 8 903

04

05

06

07

Excitation casePassive

GHFLC Optimal

J 3 J 5

Figure 15 Comparisons on the performance indexes J3and J7for different control cases

14 Mathematical Problems in Engineering

1 2 3 4 5 6 7 8 907

08

09

10

11

12

13

14

15

Excitation casePassive

GHFLC Optimal

1 2 3 4 5 6 7 8 907

08

09

10

11

12

13

Excitation case

Passive

GHFLC Optimal

J 8J 5

Figure 16 Comparison of the performance indexes J5and J8for different control cases

with piezoelectric friction dampers installed on the isolationthe energy equations are defined as follows

119864119870+ 119864120585+ 119864119878+ 119864119867= 119864119868

119864119870=1

2119879

119905119872119905

119864120585= int

119905

0

119879

119888 119889119905

119864119878= int

119905

0

119909119879

119870119889119909

119864119867= minusint

119905

0

119906119879

119864119879

119904119889119909

119864119868= minusint

119905

0

gMI 119889119909

(15)

where 119864119870 119864120585 119864119878 119864119867 and 119864

119868denote the absolute kinetic

energy damping energy elastic strain energy energy dis-sipated by piezoelectric friction dampers and total inputenergy respectively The energy time histories for differentcontrollers against TCU052Chi-Chi earthquake are shown inFigure 17 It can be seen from the figures that the piezoelectricfriction dampers dissipate most of the input energy fordifferent control cases subjected to TCU052 earthquake

In order to compare different effects under near-faultground motions recorded for different sites the average ofinput energy and structure responses subjected to near-faultearthquakes are given in Table 8

As shown in Table 8 the near-fault earthquakes forsoft sites are more destructive than hard sites For instancecompared to hard sites the input energy and the base dis-placement of RMS of the base-isolated structure for soft soil

increase by 143 and 256 respectively However GHFLCpossesses favorable performance under different ground sitesand the damping effect has no distinctly direct relationshipwith site category

As discussed in Section 61 the isolation ratio of thesimulation model equals 83 In order to evaluate the effectsof isolation ratio on the damping performance of GHFLC thestiffness value of isolation is adjusted to 1045 and 452 kNmrespectively Then the numerical results for different valuesof isolation ratio (120575 = 4 6) are obtained The performanceindexes J

3and J5for different isolation ratios are shown in

Figures 18 and 19 respectivelyFor base-isolated structure isolation ratio has a signifi-

cant influence on the isolation effect A larger isolation ratiowhich means a minor stiffness value of isolation usuallyleads to conspicuous enlargement of base displacement anddecrease of superstructural responses due to the increaseof fundamental vibration period and vice versa Howeveras shown in Figures 18 and 19 the shock absorption rateof GHFLC has little change when isolation ratio variesdifferently and the proposed fuzzy control shows favorableeffectiveness in the diverse isolation ratios of base-isolatedstructures

7 Conclusions

In this study an optimized fuzzy logic control which isdesigned for Chi-Chi near-fault earthquakes under differentground sites is proposed An elastic design spectrum isproposed to generate near-fault earthquakes for differentground sitesThe characteristic of the design spectrum is thatit has larger periods and peak acceleration than conventionalspectrum Genetic algorithm is employed to optimize thesupervisory fuzzy controller and preload of piezoelectric

Mathematical Problems in Engineering 15

Table 8 Average ofinput energy and structure responses subjected to near-fault earthquakes

Site classification Input energy (kNsdotm) Base shear (kN) Base displacement ofRMS (m)

Structure accelerationof RMS (g)

Hard soil 24375 475 0047 0432Medium soil 26746 498 0054 0476Soft soil 27857 568 0059 0531

20 30 40 50 60 7000

05

10

15

20

25

Input energyEnergy dissipated by dampers

Time (s)

Ener

gy (k

Nmiddotm

)

times104

(a) Passive control

20 30 40 50 60 7000

05

10

15

20

25

30

Time (s)

Input energyEnergy dissipated by dampers

Ener

gy (k

Nmiddotm

)

times104

(b) Optimal control

20 30 40 50 60 7000

05

10

15

20

25

30

Input energyEnergy dissipated by dampers

Time (s)

Ener

gy (k

Nmiddotm

)

times104

(c) GHFLC method

Figure 17 Energy time histories subjected to Chi-Chi TCU052 earthquake

friction dampers according to three artificial earthquakesthat are characterized by Chi-Chi earthquakes Passive andoptimal controllers are also compared with the performanceof the developed fuzzy controller The simulation resultsreveal that the developed semiactive fuzzy controller hasbetter performance than traditional passive and optimal con-troller in simultaneously reducing the base displacement and

floor acceleration under near-fault earthquakes for differentground sites

Conflict of Interests

The authors declare no conflict of interests regarding thepublication of this paper

16 Mathematical Problems in Engineering

1 2 3 4 5 6 7 8 903

04

05

06

07

08

Excitation casePassive

GHFLC Optimal

1 2 3 4 5 6 7 8 907

08

09

10

11

12

13

14

15

Excitation case

Passive

GHFLC Optimal

J 3 J 5Figure 18 Comparisons on the performance indexes J

3and J5for different control cases (120575 = 4)

1 2 3 4 5 6 7 8 903

04

05

06

07

08

Excitation casePassive

GHFLC Optimal

1 2 3 4 5 6 7 8 907

08

09

10

11

12

13

14

15

Excitation casePassive

GHFLC Optimal

J 3 J 5

Figure 19 Comparisons on the performance indexes J3and J5for different control cases (120575 = 6)

Acknowledgments

This research was supported by National Natural ScienceFoundation of China under Grant no 51308487 no 41402261and no 51408526 Hebei Provincial Natural Science Founda-tion ofChina underGrant no E2014203055 and the ExcellentYouth Foundation of Hebei Educational Committee underGrant no YQ2013015 The support for this research is greatlyappreciated

References

[1] C Alhan and H Gavin ldquoA parametric study of linear and non-linear passively damped seismic isolation systems for buildingsrdquoEngineering Structures vol 26 no 4 pp 485ndash497 2004

[2] R S Jangid and J M Kelly ldquoBase isolation for near-faultmotionsrdquoEarthquake Engineering and Structural Dynamics vol30 no 5 pp 691ndash707 2001

[3] J Shen M-H Tsai K-C Chang and G C Lee ldquoPerformanceof a seismically isolated bridge under near-fault earthquake

Mathematical Problems in Engineering 17

ground motionsrdquo Journal of Structural Engineering vol 130 no6 pp 861ndash868 2004

[4] F Mazza A Vulcano and M Mazza ldquoNonlinear dynamicresponse of RC buildings with different base Isolation systemssubjected to horizontal and vertical components of near-faultground motionsrdquo Open Construction and Building TechnologyJournal vol 6 pp 373ndash383 2012

[5] F Mazza and A Vulcano ldquoEffects of near-fault ground motionson the nonlinear dynamic response of base-isolated rc framedbuildingsrdquo Earthquake Engineering and Structural Dynamicsvol 41 no 2 pp 211ndash232 2012

[6] O E Ozbulut and S Hurlebaus ldquoFuzzy control of piezoelectricfriction dampers for seismic protection of smart base isolatedbuildingsrdquo Bulletin of Earthquake Engineering vol 8 no 6 pp1435ndash1455 2010

[7] O E Ozbulut M Bitaraf and S Hurlebaus ldquoAdaptive controlof base-isolated structures against near-field earthquakes usingvariable friction dampersrdquo Engineering Structures vol 33 no12 pp 3143ndash3154 2011

[8] J M Kelly ldquoThe role of damping in seismic isolationrdquo Earth-quake Engineering and Structural Dynamics vol 28 no 1 pp3ndash20 1999

[9] F Mazza and A Vulcano ldquoNonlinear response of RC framedbuildings with isolation and supplemental damping at the basesubjected to near-fault earthquakesrdquo Journal of EarthquakeEngineering vol 13 no 5 pp 690ndash715 2009

[10] M Bitaraf and S Hurlebaus ldquoSemi-active adaptive control ofseismically excited 20-story nonlinear buildingrdquo EngineeringStructures vol 56 no 11 pp 2107ndash2118 2013

[11] D Das T K Datta and A Madan ldquoSemiactive fuzzy controlof the seismic response of building frames with MR dampersrdquoEarthquake Engineering and Structural Dynamics vol 41 no 1pp 99ndash118 2012

[12] A-P Wang and C-D Lee ldquoFuzzy sliding mode control for abuilding structure based on genetic algorithmsrdquo EarthquakeEngineering and Structural Dynamics vol 31 no 4 pp 881ndash8952002

[13] D G Reigles and M D Symans ldquoSupervisory fuzzy controlof a base-isolated benchmark building utilizing a neuro-fuzzymodel of controllable fluid viscous dampersrdquo Structural Controland Health Monitoring vol 13 no 2-3 pp 724ndash747 2006

[14] H-S Kim and P N Roschke ldquoGA-fuzzy control of smartbase isolated benchmark building using supervisory controltechniquerdquo Advances in Engineering Software vol 38 no 7 pp453ndash465 2007

[15] D Yang and Y Zhao ldquoEffects of rupture forward directivity andfling step of near-fault groundmotions on seismic performanceof base-isolated building structurerdquo Acta Seismologica Sinicavol 32 no 5 pp 579ndash587 2010

[16] Y E-A Mohamedzein J A Abdalla and A Abdelwahab ldquoSiteresponse and earthquake design spectra for central KhartoumSudanrdquoBulletin of Earthquake Engineering vol 4 no 3 pp 277ndash293 2006

[17] D Zhao and H Li ldquoShaking table tests and analyses of semi-active fuzzy control for structural seismic reduction with apiezoelectric variable-friction damperrdquo Smart Materials andStructures vol 19 no 10 Article ID 105031 2010

[18] W L He A K Agrawal and J N Yang ldquoNovel semiactivefriction controller for linear structures against earthquakesrdquoJournal of Structural Engineering vol 129 no 7 pp 941ndash9502003

[19] J N Yang and A K Agrawal ldquoSemi-active hybrid controlsystems for nonlinear buildings against near-field earthquakesrdquoEngineering Structures vol 24 no 3 pp 271ndash280 2002

[20] O E Ozbulut and S Hurlebaus ldquoOptimal design of supere-lastic-friction base isolators for seismic protection of highwaybridges against near-field earthquakesrdquo Earthquake Engineeringand Structural Dynamics vol 40 no 3 pp 273ndash291 2011

[21] D A Shook P N Roschke and O E Ozbulut ldquoSuperelasticsemi-active damping of a base-isolated structurerdquo StructuralControl and HealthMonitoring vol 15 no 5 pp 746ndash768 2008

[22] K D PhamG JinM K Sain B F Spencer Jr and S R LibertyldquoGeneralized linear quadratic Gaussian techniques for the windbenchmark problemrdquo Journal of Engineering Mechanics vol130 no 4 pp 466ndash470 2004

[23] S Nagarajaiah and S Narasimhan ldquoSmart base-isolated bench-mark building Part II Phase I sample controllers for linearisolation systemsrdquo Structural Control and Health Monitoringvol 13 no 2-3 pp 605ndash625 2006

Submit your manuscripts athttpwwwhindawicom

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

MathematicsJournal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Mathematical Problems in Engineering

Hindawi Publishing Corporationhttpwwwhindawicom

Differential EquationsInternational Journal of

Volume 2014

Applied MathematicsJournal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Probability and StatisticsHindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Journal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Mathematical PhysicsAdvances in

Complex AnalysisJournal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

OptimizationJournal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

CombinatoricsHindawi Publishing Corporationhttpwwwhindawicom Volume 2014

International Journal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Operations ResearchAdvances in

Journal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Function Spaces

Abstract and Applied AnalysisHindawi Publishing Corporationhttpwwwhindawicom Volume 2014

International Journal of Mathematics and Mathematical Sciences

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

The Scientific World JournalHindawi Publishing Corporation httpwwwhindawicom Volume 2014

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Algebra

Discrete Dynamics in Nature and Society

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Decision SciencesAdvances in

Discrete MathematicsJournal of

Hindawi Publishing Corporationhttpwwwhindawicom

Volume 2014 Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Stochastic AnalysisInternational Journal of

12 Mathematical Problems in Engineering

Table 6 Performance index

Peak base shear Peak interstory drift RMS base displacement

1198691=max119905

10038171003817100381710038171198810 (119905)1003817100381710038171003817

max119905

100381710038171003817100381710038171198810(119905)10038171003817100381710038171003817

1198694=

max119905119891

10038171003817100381710038171003817119889119891(119905)10038171003817100381710038171003817

max119905119891

10038171003817100381710038171003817119889119891(119905)10038171003817100381710038171003817

1198697=

max119894

1003817100381710038171003817120590119889 (119905)1003817100381710038171003817

max119905

1003817100381710038171003817119889 (119905)1003817100381710038171003817

Peak structural shear Peak floor acceleration RMS floor acceleration

1198692=max119905

10038171003817100381710038171198811 (119905)1003817100381710038171003817

max119905

100381710038171003817100381710038171198811(119905)10038171003817100381710038171003817

1198695=

max119905119891

10038171003817100381710038171003817119886119891(119905)10038171003817100381710038171003817

max119905119891

10038171003817100381710038171003817119886119891(119905)10038171003817100381710038171003817

1198698=max119891

1003817100381710038171003817120590119886 (119905)1003817100381710038171003817

max119891

1003817100381710038171003817119886 (119905)1003817100381710038171003817

Peak base displacement Peak control force Energy dissipated by PFD

1198693=max119905

1003817100381710038171003817119909119887 (119905)1003817100381710038171003817

max119905

1003817100381710038171003817119909119887 (119905)1003817100381710038171003817

1198696=max119905

1003817100381710038171003817119891119889 (119905)1003817100381710038171003817

max119905

10038171003817100381710038171198810 (119905)1003817100381710038171003817

1198699=

int119879

0

119891119889(119905) 119887(119905) 119889119905

int119879

0

1198810(119905) 119892(119905) 119889119905

Table 7 Results of numerical simulation

Earthquake Control case 1198691

1198692

1198693

1198694

1198695

1198696

1198697

1198698

1198699

TCU102(hard site)

Passive 081 082 068 085 094 048 057 082 078Optimal 092 095 075 099 087 043 068 081 069GHFLC 087 091 071 093 082 041 061 078 073

TCU052(hard site)

Passive 079 079 046 082 106 036 038 089 087Optimal 087 087 057 087 098 029 049 085 079GHFLC 083 082 055 082 091 033 044 079 084

Artificialearthquake(hard site)

Passive 072 074 054 076 092 054 049 090 084Optimal 084 086 069 083 089 047 057 086 073GHFLC 076 077 061 079 083 042 052 081 076

TCU053(medium site)

Passive 061 065 039 071 145 032 037 116 089Optimal 069 072 046 076 136 031 045 117 078GHFLC 062 062 042 065 132 026 044 109 072

TCU054(medium site)

Passive 071 073 043 073 142 084 038 121 088Optimal 081 087 045 085 132 079 052 125 086GHFLC 075 071 040 074 126 082 045 113 076

Artificialearthquake(medium site)

Passive 054 057 038 064 123 067 036 117 091Optimal 067 066 047 067 119 078 048 113 079GHFLC 058 061 040 062 113 072 041 109 085

TCU110(soft soil site)

Passive 077 078 047 077 103 050 045 089 095Optimal 083 082 052 085 107 046 052 099 087GHFLC 086 086 056 086 104 042 049 093 090

CHY101(soft soil site)

Passive 069 071 058 075 086 066 054 092 084Optimal 075 073 062 074 087 064 055 088 079GHFLC 063 067 054 067 079 065 051 087 083

Artificialearthquake(soft site)

Passive 057 064 061 068 097 061 058 098 088Optimal 071 070 074 075 094 058 071 093 083GHFLC 065 062 067 069 085 055 063 086 076

controller in simultaneously depressing the superstructureacceleration and base displacement For example the appli-cation of developed fuzzy controller leads to an average of112 decrease in peak floor acceleration and an average ofonly 36 increase in peak base displacement as compared topassive control Particularly optimal controller produces anaverage of only 41 reduction in peak floor acceleration and

leads to 79 increase in peak base displacement as comparedto passive control Therefore the improved fuzzy controlmethod shows better performance than passive and optimalcontrol

In order to further evaluate the performance of differentcontrollers the energy time histories for different controllersare compared with each other For a base-isolated structure

Mathematical Problems in Engineering 13

20 30 40 50 60 70minus20

minus10

00

10

20Fr

ictio

n fo

rce (

kN)

Time (s)minus03 minus02 minus01 00 01 02 03

minus20

minus10

00

10

20

Fric

tion

forc

e (kN

)

Displacement (m)

(a) Passive control

20 30 40 50 60 70minus20

minus10

00

10

20

Fric

tion

forc

e (kN

)

Time (s)minus03 minus02 minus01 00 01 02 03

minus20

minus10

00

10

20

Fric

tion

forc

e (kN

)

Displacement (m)

(b) GHFLC method

Figure 14 Time histories of friction force and force-displacement diagram against TCU052 earthquake

1 2 3 4 5 6 7 8 903

04

05

06

07

08

Excitation case

Passive OptimalGHFLC

1 2 3 4 5 6 7 8 903

04

05

06

07

Excitation casePassive

GHFLC Optimal

J 3 J 5

Figure 15 Comparisons on the performance indexes J3and J7for different control cases

14 Mathematical Problems in Engineering

1 2 3 4 5 6 7 8 907

08

09

10

11

12

13

14

15

Excitation casePassive

GHFLC Optimal

1 2 3 4 5 6 7 8 907

08

09

10

11

12

13

Excitation case

Passive

GHFLC Optimal

J 8J 5

Figure 16 Comparison of the performance indexes J5and J8for different control cases

with piezoelectric friction dampers installed on the isolationthe energy equations are defined as follows

119864119870+ 119864120585+ 119864119878+ 119864119867= 119864119868

119864119870=1

2119879

119905119872119905

119864120585= int

119905

0

119879

119888 119889119905

119864119878= int

119905

0

119909119879

119870119889119909

119864119867= minusint

119905

0

119906119879

119864119879

119904119889119909

119864119868= minusint

119905

0

gMI 119889119909

(15)

where 119864119870 119864120585 119864119878 119864119867 and 119864

119868denote the absolute kinetic

energy damping energy elastic strain energy energy dis-sipated by piezoelectric friction dampers and total inputenergy respectively The energy time histories for differentcontrollers against TCU052Chi-Chi earthquake are shown inFigure 17 It can be seen from the figures that the piezoelectricfriction dampers dissipate most of the input energy fordifferent control cases subjected to TCU052 earthquake

In order to compare different effects under near-faultground motions recorded for different sites the average ofinput energy and structure responses subjected to near-faultearthquakes are given in Table 8

As shown in Table 8 the near-fault earthquakes forsoft sites are more destructive than hard sites For instancecompared to hard sites the input energy and the base dis-placement of RMS of the base-isolated structure for soft soil

increase by 143 and 256 respectively However GHFLCpossesses favorable performance under different ground sitesand the damping effect has no distinctly direct relationshipwith site category

As discussed in Section 61 the isolation ratio of thesimulation model equals 83 In order to evaluate the effectsof isolation ratio on the damping performance of GHFLC thestiffness value of isolation is adjusted to 1045 and 452 kNmrespectively Then the numerical results for different valuesof isolation ratio (120575 = 4 6) are obtained The performanceindexes J

3and J5for different isolation ratios are shown in

Figures 18 and 19 respectivelyFor base-isolated structure isolation ratio has a signifi-

cant influence on the isolation effect A larger isolation ratiowhich means a minor stiffness value of isolation usuallyleads to conspicuous enlargement of base displacement anddecrease of superstructural responses due to the increaseof fundamental vibration period and vice versa Howeveras shown in Figures 18 and 19 the shock absorption rateof GHFLC has little change when isolation ratio variesdifferently and the proposed fuzzy control shows favorableeffectiveness in the diverse isolation ratios of base-isolatedstructures

7 Conclusions

In this study an optimized fuzzy logic control which isdesigned for Chi-Chi near-fault earthquakes under differentground sites is proposed An elastic design spectrum isproposed to generate near-fault earthquakes for differentground sitesThe characteristic of the design spectrum is thatit has larger periods and peak acceleration than conventionalspectrum Genetic algorithm is employed to optimize thesupervisory fuzzy controller and preload of piezoelectric

Mathematical Problems in Engineering 15

Table 8 Average ofinput energy and structure responses subjected to near-fault earthquakes

Site classification Input energy (kNsdotm) Base shear (kN) Base displacement ofRMS (m)

Structure accelerationof RMS (g)

Hard soil 24375 475 0047 0432Medium soil 26746 498 0054 0476Soft soil 27857 568 0059 0531

20 30 40 50 60 7000

05

10

15

20

25

Input energyEnergy dissipated by dampers

Time (s)

Ener

gy (k

Nmiddotm

)

times104

(a) Passive control

20 30 40 50 60 7000

05

10

15

20

25

30

Time (s)

Input energyEnergy dissipated by dampers

Ener

gy (k

Nmiddotm

)

times104

(b) Optimal control

20 30 40 50 60 7000

05

10

15

20

25

30

Input energyEnergy dissipated by dampers

Time (s)

Ener

gy (k

Nmiddotm

)

times104

(c) GHFLC method

Figure 17 Energy time histories subjected to Chi-Chi TCU052 earthquake

friction dampers according to three artificial earthquakesthat are characterized by Chi-Chi earthquakes Passive andoptimal controllers are also compared with the performanceof the developed fuzzy controller The simulation resultsreveal that the developed semiactive fuzzy controller hasbetter performance than traditional passive and optimal con-troller in simultaneously reducing the base displacement and

floor acceleration under near-fault earthquakes for differentground sites

Conflict of Interests

The authors declare no conflict of interests regarding thepublication of this paper

16 Mathematical Problems in Engineering

1 2 3 4 5 6 7 8 903

04

05

06

07

08

Excitation casePassive

GHFLC Optimal

1 2 3 4 5 6 7 8 907

08

09

10

11

12

13

14

15

Excitation case

Passive

GHFLC Optimal

J 3 J 5Figure 18 Comparisons on the performance indexes J

3and J5for different control cases (120575 = 4)

1 2 3 4 5 6 7 8 903

04

05

06

07

08

Excitation casePassive

GHFLC Optimal

1 2 3 4 5 6 7 8 907

08

09

10

11

12

13

14

15

Excitation casePassive

GHFLC Optimal

J 3 J 5

Figure 19 Comparisons on the performance indexes J3and J5for different control cases (120575 = 6)

Acknowledgments

This research was supported by National Natural ScienceFoundation of China under Grant no 51308487 no 41402261and no 51408526 Hebei Provincial Natural Science Founda-tion ofChina underGrant no E2014203055 and the ExcellentYouth Foundation of Hebei Educational Committee underGrant no YQ2013015 The support for this research is greatlyappreciated

References

[1] C Alhan and H Gavin ldquoA parametric study of linear and non-linear passively damped seismic isolation systems for buildingsrdquoEngineering Structures vol 26 no 4 pp 485ndash497 2004

[2] R S Jangid and J M Kelly ldquoBase isolation for near-faultmotionsrdquoEarthquake Engineering and Structural Dynamics vol30 no 5 pp 691ndash707 2001

[3] J Shen M-H Tsai K-C Chang and G C Lee ldquoPerformanceof a seismically isolated bridge under near-fault earthquake

Mathematical Problems in Engineering 17

ground motionsrdquo Journal of Structural Engineering vol 130 no6 pp 861ndash868 2004

[4] F Mazza A Vulcano and M Mazza ldquoNonlinear dynamicresponse of RC buildings with different base Isolation systemssubjected to horizontal and vertical components of near-faultground motionsrdquo Open Construction and Building TechnologyJournal vol 6 pp 373ndash383 2012

[5] F Mazza and A Vulcano ldquoEffects of near-fault ground motionson the nonlinear dynamic response of base-isolated rc framedbuildingsrdquo Earthquake Engineering and Structural Dynamicsvol 41 no 2 pp 211ndash232 2012

[6] O E Ozbulut and S Hurlebaus ldquoFuzzy control of piezoelectricfriction dampers for seismic protection of smart base isolatedbuildingsrdquo Bulletin of Earthquake Engineering vol 8 no 6 pp1435ndash1455 2010

[7] O E Ozbulut M Bitaraf and S Hurlebaus ldquoAdaptive controlof base-isolated structures against near-field earthquakes usingvariable friction dampersrdquo Engineering Structures vol 33 no12 pp 3143ndash3154 2011

[8] J M Kelly ldquoThe role of damping in seismic isolationrdquo Earth-quake Engineering and Structural Dynamics vol 28 no 1 pp3ndash20 1999

[9] F Mazza and A Vulcano ldquoNonlinear response of RC framedbuildings with isolation and supplemental damping at the basesubjected to near-fault earthquakesrdquo Journal of EarthquakeEngineering vol 13 no 5 pp 690ndash715 2009

[10] M Bitaraf and S Hurlebaus ldquoSemi-active adaptive control ofseismically excited 20-story nonlinear buildingrdquo EngineeringStructures vol 56 no 11 pp 2107ndash2118 2013

[11] D Das T K Datta and A Madan ldquoSemiactive fuzzy controlof the seismic response of building frames with MR dampersrdquoEarthquake Engineering and Structural Dynamics vol 41 no 1pp 99ndash118 2012

[12] A-P Wang and C-D Lee ldquoFuzzy sliding mode control for abuilding structure based on genetic algorithmsrdquo EarthquakeEngineering and Structural Dynamics vol 31 no 4 pp 881ndash8952002

[13] D G Reigles and M D Symans ldquoSupervisory fuzzy controlof a base-isolated benchmark building utilizing a neuro-fuzzymodel of controllable fluid viscous dampersrdquo Structural Controland Health Monitoring vol 13 no 2-3 pp 724ndash747 2006

[14] H-S Kim and P N Roschke ldquoGA-fuzzy control of smartbase isolated benchmark building using supervisory controltechniquerdquo Advances in Engineering Software vol 38 no 7 pp453ndash465 2007

[15] D Yang and Y Zhao ldquoEffects of rupture forward directivity andfling step of near-fault groundmotions on seismic performanceof base-isolated building structurerdquo Acta Seismologica Sinicavol 32 no 5 pp 579ndash587 2010

[16] Y E-A Mohamedzein J A Abdalla and A Abdelwahab ldquoSiteresponse and earthquake design spectra for central KhartoumSudanrdquoBulletin of Earthquake Engineering vol 4 no 3 pp 277ndash293 2006

[17] D Zhao and H Li ldquoShaking table tests and analyses of semi-active fuzzy control for structural seismic reduction with apiezoelectric variable-friction damperrdquo Smart Materials andStructures vol 19 no 10 Article ID 105031 2010

[18] W L He A K Agrawal and J N Yang ldquoNovel semiactivefriction controller for linear structures against earthquakesrdquoJournal of Structural Engineering vol 129 no 7 pp 941ndash9502003

[19] J N Yang and A K Agrawal ldquoSemi-active hybrid controlsystems for nonlinear buildings against near-field earthquakesrdquoEngineering Structures vol 24 no 3 pp 271ndash280 2002

[20] O E Ozbulut and S Hurlebaus ldquoOptimal design of supere-lastic-friction base isolators for seismic protection of highwaybridges against near-field earthquakesrdquo Earthquake Engineeringand Structural Dynamics vol 40 no 3 pp 273ndash291 2011

[21] D A Shook P N Roschke and O E Ozbulut ldquoSuperelasticsemi-active damping of a base-isolated structurerdquo StructuralControl and HealthMonitoring vol 15 no 5 pp 746ndash768 2008

[22] K D PhamG JinM K Sain B F Spencer Jr and S R LibertyldquoGeneralized linear quadratic Gaussian techniques for the windbenchmark problemrdquo Journal of Engineering Mechanics vol130 no 4 pp 466ndash470 2004

[23] S Nagarajaiah and S Narasimhan ldquoSmart base-isolated bench-mark building Part II Phase I sample controllers for linearisolation systemsrdquo Structural Control and Health Monitoringvol 13 no 2-3 pp 605ndash625 2006

Submit your manuscripts athttpwwwhindawicom

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

MathematicsJournal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Mathematical Problems in Engineering

Hindawi Publishing Corporationhttpwwwhindawicom

Differential EquationsInternational Journal of

Volume 2014

Applied MathematicsJournal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Probability and StatisticsHindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Journal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Mathematical PhysicsAdvances in

Complex AnalysisJournal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

OptimizationJournal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

CombinatoricsHindawi Publishing Corporationhttpwwwhindawicom Volume 2014

International Journal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Operations ResearchAdvances in

Journal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Function Spaces

Abstract and Applied AnalysisHindawi Publishing Corporationhttpwwwhindawicom Volume 2014

International Journal of Mathematics and Mathematical Sciences

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

The Scientific World JournalHindawi Publishing Corporation httpwwwhindawicom Volume 2014

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Algebra

Discrete Dynamics in Nature and Society

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Decision SciencesAdvances in

Discrete MathematicsJournal of

Hindawi Publishing Corporationhttpwwwhindawicom

Volume 2014 Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Stochastic AnalysisInternational Journal of

Mathematical Problems in Engineering 13

20 30 40 50 60 70minus20

minus10

00

10

20Fr

ictio

n fo

rce (

kN)

Time (s)minus03 minus02 minus01 00 01 02 03

minus20

minus10

00

10

20

Fric

tion

forc

e (kN

)

Displacement (m)

(a) Passive control

20 30 40 50 60 70minus20

minus10

00

10

20

Fric

tion

forc

e (kN

)

Time (s)minus03 minus02 minus01 00 01 02 03

minus20

minus10

00

10

20

Fric

tion

forc

e (kN

)

Displacement (m)

(b) GHFLC method

Figure 14 Time histories of friction force and force-displacement diagram against TCU052 earthquake

1 2 3 4 5 6 7 8 903

04

05

06

07

08

Excitation case

Passive OptimalGHFLC

1 2 3 4 5 6 7 8 903

04

05

06

07

Excitation casePassive

GHFLC Optimal

J 3 J 5

Figure 15 Comparisons on the performance indexes J3and J7for different control cases

14 Mathematical Problems in Engineering

1 2 3 4 5 6 7 8 907

08

09

10

11

12

13

14

15

Excitation casePassive

GHFLC Optimal

1 2 3 4 5 6 7 8 907

08

09

10

11

12

13

Excitation case

Passive

GHFLC Optimal

J 8J 5

Figure 16 Comparison of the performance indexes J5and J8for different control cases

with piezoelectric friction dampers installed on the isolationthe energy equations are defined as follows

119864119870+ 119864120585+ 119864119878+ 119864119867= 119864119868

119864119870=1

2119879

119905119872119905

119864120585= int

119905

0

119879

119888 119889119905

119864119878= int

119905

0

119909119879

119870119889119909

119864119867= minusint

119905

0

119906119879

119864119879

119904119889119909

119864119868= minusint

119905

0

gMI 119889119909

(15)

where 119864119870 119864120585 119864119878 119864119867 and 119864

119868denote the absolute kinetic

energy damping energy elastic strain energy energy dis-sipated by piezoelectric friction dampers and total inputenergy respectively The energy time histories for differentcontrollers against TCU052Chi-Chi earthquake are shown inFigure 17 It can be seen from the figures that the piezoelectricfriction dampers dissipate most of the input energy fordifferent control cases subjected to TCU052 earthquake

In order to compare different effects under near-faultground motions recorded for different sites the average ofinput energy and structure responses subjected to near-faultearthquakes are given in Table 8

As shown in Table 8 the near-fault earthquakes forsoft sites are more destructive than hard sites For instancecompared to hard sites the input energy and the base dis-placement of RMS of the base-isolated structure for soft soil

increase by 143 and 256 respectively However GHFLCpossesses favorable performance under different ground sitesand the damping effect has no distinctly direct relationshipwith site category

As discussed in Section 61 the isolation ratio of thesimulation model equals 83 In order to evaluate the effectsof isolation ratio on the damping performance of GHFLC thestiffness value of isolation is adjusted to 1045 and 452 kNmrespectively Then the numerical results for different valuesof isolation ratio (120575 = 4 6) are obtained The performanceindexes J

3and J5for different isolation ratios are shown in

Figures 18 and 19 respectivelyFor base-isolated structure isolation ratio has a signifi-

cant influence on the isolation effect A larger isolation ratiowhich means a minor stiffness value of isolation usuallyleads to conspicuous enlargement of base displacement anddecrease of superstructural responses due to the increaseof fundamental vibration period and vice versa Howeveras shown in Figures 18 and 19 the shock absorption rateof GHFLC has little change when isolation ratio variesdifferently and the proposed fuzzy control shows favorableeffectiveness in the diverse isolation ratios of base-isolatedstructures

7 Conclusions

In this study an optimized fuzzy logic control which isdesigned for Chi-Chi near-fault earthquakes under differentground sites is proposed An elastic design spectrum isproposed to generate near-fault earthquakes for differentground sitesThe characteristic of the design spectrum is thatit has larger periods and peak acceleration than conventionalspectrum Genetic algorithm is employed to optimize thesupervisory fuzzy controller and preload of piezoelectric

Mathematical Problems in Engineering 15

Table 8 Average ofinput energy and structure responses subjected to near-fault earthquakes

Site classification Input energy (kNsdotm) Base shear (kN) Base displacement ofRMS (m)

Structure accelerationof RMS (g)

Hard soil 24375 475 0047 0432Medium soil 26746 498 0054 0476Soft soil 27857 568 0059 0531

20 30 40 50 60 7000

05

10

15

20

25

Input energyEnergy dissipated by dampers

Time (s)

Ener

gy (k

Nmiddotm

)

times104

(a) Passive control

20 30 40 50 60 7000

05

10

15

20

25

30

Time (s)

Input energyEnergy dissipated by dampers

Ener

gy (k

Nmiddotm

)

times104

(b) Optimal control

20 30 40 50 60 7000

05

10

15

20

25

30

Input energyEnergy dissipated by dampers

Time (s)

Ener

gy (k

Nmiddotm

)

times104

(c) GHFLC method

Figure 17 Energy time histories subjected to Chi-Chi TCU052 earthquake

friction dampers according to three artificial earthquakesthat are characterized by Chi-Chi earthquakes Passive andoptimal controllers are also compared with the performanceof the developed fuzzy controller The simulation resultsreveal that the developed semiactive fuzzy controller hasbetter performance than traditional passive and optimal con-troller in simultaneously reducing the base displacement and

floor acceleration under near-fault earthquakes for differentground sites

Conflict of Interests

The authors declare no conflict of interests regarding thepublication of this paper

16 Mathematical Problems in Engineering

1 2 3 4 5 6 7 8 903

04

05

06

07

08

Excitation casePassive

GHFLC Optimal

1 2 3 4 5 6 7 8 907

08

09

10

11

12

13

14

15

Excitation case

Passive

GHFLC Optimal

J 3 J 5Figure 18 Comparisons on the performance indexes J

3and J5for different control cases (120575 = 4)

1 2 3 4 5 6 7 8 903

04

05

06

07

08

Excitation casePassive

GHFLC Optimal

1 2 3 4 5 6 7 8 907

08

09

10

11

12

13

14

15

Excitation casePassive

GHFLC Optimal

J 3 J 5

Figure 19 Comparisons on the performance indexes J3and J5for different control cases (120575 = 6)

Acknowledgments

This research was supported by National Natural ScienceFoundation of China under Grant no 51308487 no 41402261and no 51408526 Hebei Provincial Natural Science Founda-tion ofChina underGrant no E2014203055 and the ExcellentYouth Foundation of Hebei Educational Committee underGrant no YQ2013015 The support for this research is greatlyappreciated

References

[1] C Alhan and H Gavin ldquoA parametric study of linear and non-linear passively damped seismic isolation systems for buildingsrdquoEngineering Structures vol 26 no 4 pp 485ndash497 2004

[2] R S Jangid and J M Kelly ldquoBase isolation for near-faultmotionsrdquoEarthquake Engineering and Structural Dynamics vol30 no 5 pp 691ndash707 2001

[3] J Shen M-H Tsai K-C Chang and G C Lee ldquoPerformanceof a seismically isolated bridge under near-fault earthquake

Mathematical Problems in Engineering 17

ground motionsrdquo Journal of Structural Engineering vol 130 no6 pp 861ndash868 2004

[4] F Mazza A Vulcano and M Mazza ldquoNonlinear dynamicresponse of RC buildings with different base Isolation systemssubjected to horizontal and vertical components of near-faultground motionsrdquo Open Construction and Building TechnologyJournal vol 6 pp 373ndash383 2012

[5] F Mazza and A Vulcano ldquoEffects of near-fault ground motionson the nonlinear dynamic response of base-isolated rc framedbuildingsrdquo Earthquake Engineering and Structural Dynamicsvol 41 no 2 pp 211ndash232 2012

[6] O E Ozbulut and S Hurlebaus ldquoFuzzy control of piezoelectricfriction dampers for seismic protection of smart base isolatedbuildingsrdquo Bulletin of Earthquake Engineering vol 8 no 6 pp1435ndash1455 2010

[7] O E Ozbulut M Bitaraf and S Hurlebaus ldquoAdaptive controlof base-isolated structures against near-field earthquakes usingvariable friction dampersrdquo Engineering Structures vol 33 no12 pp 3143ndash3154 2011

[8] J M Kelly ldquoThe role of damping in seismic isolationrdquo Earth-quake Engineering and Structural Dynamics vol 28 no 1 pp3ndash20 1999

[9] F Mazza and A Vulcano ldquoNonlinear response of RC framedbuildings with isolation and supplemental damping at the basesubjected to near-fault earthquakesrdquo Journal of EarthquakeEngineering vol 13 no 5 pp 690ndash715 2009

[10] M Bitaraf and S Hurlebaus ldquoSemi-active adaptive control ofseismically excited 20-story nonlinear buildingrdquo EngineeringStructures vol 56 no 11 pp 2107ndash2118 2013

[11] D Das T K Datta and A Madan ldquoSemiactive fuzzy controlof the seismic response of building frames with MR dampersrdquoEarthquake Engineering and Structural Dynamics vol 41 no 1pp 99ndash118 2012

[12] A-P Wang and C-D Lee ldquoFuzzy sliding mode control for abuilding structure based on genetic algorithmsrdquo EarthquakeEngineering and Structural Dynamics vol 31 no 4 pp 881ndash8952002

[13] D G Reigles and M D Symans ldquoSupervisory fuzzy controlof a base-isolated benchmark building utilizing a neuro-fuzzymodel of controllable fluid viscous dampersrdquo Structural Controland Health Monitoring vol 13 no 2-3 pp 724ndash747 2006

[14] H-S Kim and P N Roschke ldquoGA-fuzzy control of smartbase isolated benchmark building using supervisory controltechniquerdquo Advances in Engineering Software vol 38 no 7 pp453ndash465 2007

[15] D Yang and Y Zhao ldquoEffects of rupture forward directivity andfling step of near-fault groundmotions on seismic performanceof base-isolated building structurerdquo Acta Seismologica Sinicavol 32 no 5 pp 579ndash587 2010

[16] Y E-A Mohamedzein J A Abdalla and A Abdelwahab ldquoSiteresponse and earthquake design spectra for central KhartoumSudanrdquoBulletin of Earthquake Engineering vol 4 no 3 pp 277ndash293 2006

[17] D Zhao and H Li ldquoShaking table tests and analyses of semi-active fuzzy control for structural seismic reduction with apiezoelectric variable-friction damperrdquo Smart Materials andStructures vol 19 no 10 Article ID 105031 2010

[18] W L He A K Agrawal and J N Yang ldquoNovel semiactivefriction controller for linear structures against earthquakesrdquoJournal of Structural Engineering vol 129 no 7 pp 941ndash9502003

[19] J N Yang and A K Agrawal ldquoSemi-active hybrid controlsystems for nonlinear buildings against near-field earthquakesrdquoEngineering Structures vol 24 no 3 pp 271ndash280 2002

[20] O E Ozbulut and S Hurlebaus ldquoOptimal design of supere-lastic-friction base isolators for seismic protection of highwaybridges against near-field earthquakesrdquo Earthquake Engineeringand Structural Dynamics vol 40 no 3 pp 273ndash291 2011

[21] D A Shook P N Roschke and O E Ozbulut ldquoSuperelasticsemi-active damping of a base-isolated structurerdquo StructuralControl and HealthMonitoring vol 15 no 5 pp 746ndash768 2008

[22] K D PhamG JinM K Sain B F Spencer Jr and S R LibertyldquoGeneralized linear quadratic Gaussian techniques for the windbenchmark problemrdquo Journal of Engineering Mechanics vol130 no 4 pp 466ndash470 2004

[23] S Nagarajaiah and S Narasimhan ldquoSmart base-isolated bench-mark building Part II Phase I sample controllers for linearisolation systemsrdquo Structural Control and Health Monitoringvol 13 no 2-3 pp 605ndash625 2006

Submit your manuscripts athttpwwwhindawicom

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

MathematicsJournal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Mathematical Problems in Engineering

Hindawi Publishing Corporationhttpwwwhindawicom

Differential EquationsInternational Journal of

Volume 2014

Applied MathematicsJournal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Probability and StatisticsHindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Journal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Mathematical PhysicsAdvances in

Complex AnalysisJournal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

OptimizationJournal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

CombinatoricsHindawi Publishing Corporationhttpwwwhindawicom Volume 2014

International Journal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Operations ResearchAdvances in

Journal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Function Spaces

Abstract and Applied AnalysisHindawi Publishing Corporationhttpwwwhindawicom Volume 2014

International Journal of Mathematics and Mathematical Sciences

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

The Scientific World JournalHindawi Publishing Corporation httpwwwhindawicom Volume 2014

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Algebra

Discrete Dynamics in Nature and Society

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Decision SciencesAdvances in

Discrete MathematicsJournal of

Hindawi Publishing Corporationhttpwwwhindawicom

Volume 2014 Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Stochastic AnalysisInternational Journal of

14 Mathematical Problems in Engineering

1 2 3 4 5 6 7 8 907

08

09

10

11

12

13

14

15

Excitation casePassive

GHFLC Optimal

1 2 3 4 5 6 7 8 907

08

09

10

11

12

13

Excitation case

Passive

GHFLC Optimal

J 8J 5

Figure 16 Comparison of the performance indexes J5and J8for different control cases

with piezoelectric friction dampers installed on the isolationthe energy equations are defined as follows

119864119870+ 119864120585+ 119864119878+ 119864119867= 119864119868

119864119870=1

2119879

119905119872119905

119864120585= int

119905

0

119879

119888 119889119905

119864119878= int

119905

0

119909119879

119870119889119909

119864119867= minusint

119905

0

119906119879

119864119879

119904119889119909

119864119868= minusint

119905

0

gMI 119889119909

(15)

where 119864119870 119864120585 119864119878 119864119867 and 119864

119868denote the absolute kinetic

energy damping energy elastic strain energy energy dis-sipated by piezoelectric friction dampers and total inputenergy respectively The energy time histories for differentcontrollers against TCU052Chi-Chi earthquake are shown inFigure 17 It can be seen from the figures that the piezoelectricfriction dampers dissipate most of the input energy fordifferent control cases subjected to TCU052 earthquake

In order to compare different effects under near-faultground motions recorded for different sites the average ofinput energy and structure responses subjected to near-faultearthquakes are given in Table 8

As shown in Table 8 the near-fault earthquakes forsoft sites are more destructive than hard sites For instancecompared to hard sites the input energy and the base dis-placement of RMS of the base-isolated structure for soft soil

increase by 143 and 256 respectively However GHFLCpossesses favorable performance under different ground sitesand the damping effect has no distinctly direct relationshipwith site category

As discussed in Section 61 the isolation ratio of thesimulation model equals 83 In order to evaluate the effectsof isolation ratio on the damping performance of GHFLC thestiffness value of isolation is adjusted to 1045 and 452 kNmrespectively Then the numerical results for different valuesof isolation ratio (120575 = 4 6) are obtained The performanceindexes J

3and J5for different isolation ratios are shown in

Figures 18 and 19 respectivelyFor base-isolated structure isolation ratio has a signifi-

cant influence on the isolation effect A larger isolation ratiowhich means a minor stiffness value of isolation usuallyleads to conspicuous enlargement of base displacement anddecrease of superstructural responses due to the increaseof fundamental vibration period and vice versa Howeveras shown in Figures 18 and 19 the shock absorption rateof GHFLC has little change when isolation ratio variesdifferently and the proposed fuzzy control shows favorableeffectiveness in the diverse isolation ratios of base-isolatedstructures

7 Conclusions

In this study an optimized fuzzy logic control which isdesigned for Chi-Chi near-fault earthquakes under differentground sites is proposed An elastic design spectrum isproposed to generate near-fault earthquakes for differentground sitesThe characteristic of the design spectrum is thatit has larger periods and peak acceleration than conventionalspectrum Genetic algorithm is employed to optimize thesupervisory fuzzy controller and preload of piezoelectric

Mathematical Problems in Engineering 15

Table 8 Average ofinput energy and structure responses subjected to near-fault earthquakes

Site classification Input energy (kNsdotm) Base shear (kN) Base displacement ofRMS (m)

Structure accelerationof RMS (g)

Hard soil 24375 475 0047 0432Medium soil 26746 498 0054 0476Soft soil 27857 568 0059 0531

20 30 40 50 60 7000

05

10

15

20

25

Input energyEnergy dissipated by dampers

Time (s)

Ener

gy (k

Nmiddotm

)

times104

(a) Passive control

20 30 40 50 60 7000

05

10

15

20

25

30

Time (s)

Input energyEnergy dissipated by dampers

Ener

gy (k

Nmiddotm

)

times104

(b) Optimal control

20 30 40 50 60 7000

05

10

15

20

25

30

Input energyEnergy dissipated by dampers

Time (s)

Ener

gy (k

Nmiddotm

)

times104

(c) GHFLC method

Figure 17 Energy time histories subjected to Chi-Chi TCU052 earthquake

friction dampers according to three artificial earthquakesthat are characterized by Chi-Chi earthquakes Passive andoptimal controllers are also compared with the performanceof the developed fuzzy controller The simulation resultsreveal that the developed semiactive fuzzy controller hasbetter performance than traditional passive and optimal con-troller in simultaneously reducing the base displacement and

floor acceleration under near-fault earthquakes for differentground sites

Conflict of Interests

The authors declare no conflict of interests regarding thepublication of this paper

16 Mathematical Problems in Engineering

1 2 3 4 5 6 7 8 903

04

05

06

07

08

Excitation casePassive

GHFLC Optimal

1 2 3 4 5 6 7 8 907

08

09

10

11

12

13

14

15

Excitation case

Passive

GHFLC Optimal

J 3 J 5Figure 18 Comparisons on the performance indexes J

3and J5for different control cases (120575 = 4)

1 2 3 4 5 6 7 8 903

04

05

06

07

08

Excitation casePassive

GHFLC Optimal

1 2 3 4 5 6 7 8 907

08

09

10

11

12

13

14

15

Excitation casePassive

GHFLC Optimal

J 3 J 5

Figure 19 Comparisons on the performance indexes J3and J5for different control cases (120575 = 6)

Acknowledgments

This research was supported by National Natural ScienceFoundation of China under Grant no 51308487 no 41402261and no 51408526 Hebei Provincial Natural Science Founda-tion ofChina underGrant no E2014203055 and the ExcellentYouth Foundation of Hebei Educational Committee underGrant no YQ2013015 The support for this research is greatlyappreciated

References

[1] C Alhan and H Gavin ldquoA parametric study of linear and non-linear passively damped seismic isolation systems for buildingsrdquoEngineering Structures vol 26 no 4 pp 485ndash497 2004

[2] R S Jangid and J M Kelly ldquoBase isolation for near-faultmotionsrdquoEarthquake Engineering and Structural Dynamics vol30 no 5 pp 691ndash707 2001

[3] J Shen M-H Tsai K-C Chang and G C Lee ldquoPerformanceof a seismically isolated bridge under near-fault earthquake

Mathematical Problems in Engineering 17

ground motionsrdquo Journal of Structural Engineering vol 130 no6 pp 861ndash868 2004

[4] F Mazza A Vulcano and M Mazza ldquoNonlinear dynamicresponse of RC buildings with different base Isolation systemssubjected to horizontal and vertical components of near-faultground motionsrdquo Open Construction and Building TechnologyJournal vol 6 pp 373ndash383 2012

[5] F Mazza and A Vulcano ldquoEffects of near-fault ground motionson the nonlinear dynamic response of base-isolated rc framedbuildingsrdquo Earthquake Engineering and Structural Dynamicsvol 41 no 2 pp 211ndash232 2012

[6] O E Ozbulut and S Hurlebaus ldquoFuzzy control of piezoelectricfriction dampers for seismic protection of smart base isolatedbuildingsrdquo Bulletin of Earthquake Engineering vol 8 no 6 pp1435ndash1455 2010

[7] O E Ozbulut M Bitaraf and S Hurlebaus ldquoAdaptive controlof base-isolated structures against near-field earthquakes usingvariable friction dampersrdquo Engineering Structures vol 33 no12 pp 3143ndash3154 2011

[8] J M Kelly ldquoThe role of damping in seismic isolationrdquo Earth-quake Engineering and Structural Dynamics vol 28 no 1 pp3ndash20 1999

[9] F Mazza and A Vulcano ldquoNonlinear response of RC framedbuildings with isolation and supplemental damping at the basesubjected to near-fault earthquakesrdquo Journal of EarthquakeEngineering vol 13 no 5 pp 690ndash715 2009

[10] M Bitaraf and S Hurlebaus ldquoSemi-active adaptive control ofseismically excited 20-story nonlinear buildingrdquo EngineeringStructures vol 56 no 11 pp 2107ndash2118 2013

[11] D Das T K Datta and A Madan ldquoSemiactive fuzzy controlof the seismic response of building frames with MR dampersrdquoEarthquake Engineering and Structural Dynamics vol 41 no 1pp 99ndash118 2012

[12] A-P Wang and C-D Lee ldquoFuzzy sliding mode control for abuilding structure based on genetic algorithmsrdquo EarthquakeEngineering and Structural Dynamics vol 31 no 4 pp 881ndash8952002

[13] D G Reigles and M D Symans ldquoSupervisory fuzzy controlof a base-isolated benchmark building utilizing a neuro-fuzzymodel of controllable fluid viscous dampersrdquo Structural Controland Health Monitoring vol 13 no 2-3 pp 724ndash747 2006

[14] H-S Kim and P N Roschke ldquoGA-fuzzy control of smartbase isolated benchmark building using supervisory controltechniquerdquo Advances in Engineering Software vol 38 no 7 pp453ndash465 2007

[15] D Yang and Y Zhao ldquoEffects of rupture forward directivity andfling step of near-fault groundmotions on seismic performanceof base-isolated building structurerdquo Acta Seismologica Sinicavol 32 no 5 pp 579ndash587 2010

[16] Y E-A Mohamedzein J A Abdalla and A Abdelwahab ldquoSiteresponse and earthquake design spectra for central KhartoumSudanrdquoBulletin of Earthquake Engineering vol 4 no 3 pp 277ndash293 2006

[17] D Zhao and H Li ldquoShaking table tests and analyses of semi-active fuzzy control for structural seismic reduction with apiezoelectric variable-friction damperrdquo Smart Materials andStructures vol 19 no 10 Article ID 105031 2010

[18] W L He A K Agrawal and J N Yang ldquoNovel semiactivefriction controller for linear structures against earthquakesrdquoJournal of Structural Engineering vol 129 no 7 pp 941ndash9502003

[19] J N Yang and A K Agrawal ldquoSemi-active hybrid controlsystems for nonlinear buildings against near-field earthquakesrdquoEngineering Structures vol 24 no 3 pp 271ndash280 2002

[20] O E Ozbulut and S Hurlebaus ldquoOptimal design of supere-lastic-friction base isolators for seismic protection of highwaybridges against near-field earthquakesrdquo Earthquake Engineeringand Structural Dynamics vol 40 no 3 pp 273ndash291 2011

[21] D A Shook P N Roschke and O E Ozbulut ldquoSuperelasticsemi-active damping of a base-isolated structurerdquo StructuralControl and HealthMonitoring vol 15 no 5 pp 746ndash768 2008

[22] K D PhamG JinM K Sain B F Spencer Jr and S R LibertyldquoGeneralized linear quadratic Gaussian techniques for the windbenchmark problemrdquo Journal of Engineering Mechanics vol130 no 4 pp 466ndash470 2004

[23] S Nagarajaiah and S Narasimhan ldquoSmart base-isolated bench-mark building Part II Phase I sample controllers for linearisolation systemsrdquo Structural Control and Health Monitoringvol 13 no 2-3 pp 605ndash625 2006

Submit your manuscripts athttpwwwhindawicom

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

MathematicsJournal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Mathematical Problems in Engineering

Hindawi Publishing Corporationhttpwwwhindawicom

Differential EquationsInternational Journal of

Volume 2014

Applied MathematicsJournal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Probability and StatisticsHindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Journal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Mathematical PhysicsAdvances in

Complex AnalysisJournal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

OptimizationJournal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

CombinatoricsHindawi Publishing Corporationhttpwwwhindawicom Volume 2014

International Journal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Operations ResearchAdvances in

Journal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Function Spaces

Abstract and Applied AnalysisHindawi Publishing Corporationhttpwwwhindawicom Volume 2014

International Journal of Mathematics and Mathematical Sciences

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

The Scientific World JournalHindawi Publishing Corporation httpwwwhindawicom Volume 2014

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Algebra

Discrete Dynamics in Nature and Society

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Decision SciencesAdvances in

Discrete MathematicsJournal of

Hindawi Publishing Corporationhttpwwwhindawicom

Volume 2014 Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Stochastic AnalysisInternational Journal of

Mathematical Problems in Engineering 15

Table 8 Average ofinput energy and structure responses subjected to near-fault earthquakes

Site classification Input energy (kNsdotm) Base shear (kN) Base displacement ofRMS (m)

Structure accelerationof RMS (g)

Hard soil 24375 475 0047 0432Medium soil 26746 498 0054 0476Soft soil 27857 568 0059 0531

20 30 40 50 60 7000

05

10

15

20

25

Input energyEnergy dissipated by dampers

Time (s)

Ener

gy (k

Nmiddotm

)

times104

(a) Passive control

20 30 40 50 60 7000

05

10

15

20

25

30

Time (s)

Input energyEnergy dissipated by dampers

Ener

gy (k

Nmiddotm

)

times104

(b) Optimal control

20 30 40 50 60 7000

05

10

15

20

25

30

Input energyEnergy dissipated by dampers

Time (s)

Ener

gy (k

Nmiddotm

)

times104

(c) GHFLC method

Figure 17 Energy time histories subjected to Chi-Chi TCU052 earthquake

friction dampers according to three artificial earthquakesthat are characterized by Chi-Chi earthquakes Passive andoptimal controllers are also compared with the performanceof the developed fuzzy controller The simulation resultsreveal that the developed semiactive fuzzy controller hasbetter performance than traditional passive and optimal con-troller in simultaneously reducing the base displacement and

floor acceleration under near-fault earthquakes for differentground sites

Conflict of Interests

The authors declare no conflict of interests regarding thepublication of this paper

16 Mathematical Problems in Engineering

1 2 3 4 5 6 7 8 903

04

05

06

07

08

Excitation casePassive

GHFLC Optimal

1 2 3 4 5 6 7 8 907

08

09

10

11

12

13

14

15

Excitation case

Passive

GHFLC Optimal

J 3 J 5Figure 18 Comparisons on the performance indexes J

3and J5for different control cases (120575 = 4)

1 2 3 4 5 6 7 8 903

04

05

06

07

08

Excitation casePassive

GHFLC Optimal

1 2 3 4 5 6 7 8 907

08

09

10

11

12

13

14

15

Excitation casePassive

GHFLC Optimal

J 3 J 5

Figure 19 Comparisons on the performance indexes J3and J5for different control cases (120575 = 6)

Acknowledgments

This research was supported by National Natural ScienceFoundation of China under Grant no 51308487 no 41402261and no 51408526 Hebei Provincial Natural Science Founda-tion ofChina underGrant no E2014203055 and the ExcellentYouth Foundation of Hebei Educational Committee underGrant no YQ2013015 The support for this research is greatlyappreciated

References

[1] C Alhan and H Gavin ldquoA parametric study of linear and non-linear passively damped seismic isolation systems for buildingsrdquoEngineering Structures vol 26 no 4 pp 485ndash497 2004

[2] R S Jangid and J M Kelly ldquoBase isolation for near-faultmotionsrdquoEarthquake Engineering and Structural Dynamics vol30 no 5 pp 691ndash707 2001

[3] J Shen M-H Tsai K-C Chang and G C Lee ldquoPerformanceof a seismically isolated bridge under near-fault earthquake

Mathematical Problems in Engineering 17

ground motionsrdquo Journal of Structural Engineering vol 130 no6 pp 861ndash868 2004

[4] F Mazza A Vulcano and M Mazza ldquoNonlinear dynamicresponse of RC buildings with different base Isolation systemssubjected to horizontal and vertical components of near-faultground motionsrdquo Open Construction and Building TechnologyJournal vol 6 pp 373ndash383 2012

[5] F Mazza and A Vulcano ldquoEffects of near-fault ground motionson the nonlinear dynamic response of base-isolated rc framedbuildingsrdquo Earthquake Engineering and Structural Dynamicsvol 41 no 2 pp 211ndash232 2012

[6] O E Ozbulut and S Hurlebaus ldquoFuzzy control of piezoelectricfriction dampers for seismic protection of smart base isolatedbuildingsrdquo Bulletin of Earthquake Engineering vol 8 no 6 pp1435ndash1455 2010

[7] O E Ozbulut M Bitaraf and S Hurlebaus ldquoAdaptive controlof base-isolated structures against near-field earthquakes usingvariable friction dampersrdquo Engineering Structures vol 33 no12 pp 3143ndash3154 2011

[8] J M Kelly ldquoThe role of damping in seismic isolationrdquo Earth-quake Engineering and Structural Dynamics vol 28 no 1 pp3ndash20 1999

[9] F Mazza and A Vulcano ldquoNonlinear response of RC framedbuildings with isolation and supplemental damping at the basesubjected to near-fault earthquakesrdquo Journal of EarthquakeEngineering vol 13 no 5 pp 690ndash715 2009

[10] M Bitaraf and S Hurlebaus ldquoSemi-active adaptive control ofseismically excited 20-story nonlinear buildingrdquo EngineeringStructures vol 56 no 11 pp 2107ndash2118 2013

[11] D Das T K Datta and A Madan ldquoSemiactive fuzzy controlof the seismic response of building frames with MR dampersrdquoEarthquake Engineering and Structural Dynamics vol 41 no 1pp 99ndash118 2012

[12] A-P Wang and C-D Lee ldquoFuzzy sliding mode control for abuilding structure based on genetic algorithmsrdquo EarthquakeEngineering and Structural Dynamics vol 31 no 4 pp 881ndash8952002

[13] D G Reigles and M D Symans ldquoSupervisory fuzzy controlof a base-isolated benchmark building utilizing a neuro-fuzzymodel of controllable fluid viscous dampersrdquo Structural Controland Health Monitoring vol 13 no 2-3 pp 724ndash747 2006

[14] H-S Kim and P N Roschke ldquoGA-fuzzy control of smartbase isolated benchmark building using supervisory controltechniquerdquo Advances in Engineering Software vol 38 no 7 pp453ndash465 2007

[15] D Yang and Y Zhao ldquoEffects of rupture forward directivity andfling step of near-fault groundmotions on seismic performanceof base-isolated building structurerdquo Acta Seismologica Sinicavol 32 no 5 pp 579ndash587 2010

[16] Y E-A Mohamedzein J A Abdalla and A Abdelwahab ldquoSiteresponse and earthquake design spectra for central KhartoumSudanrdquoBulletin of Earthquake Engineering vol 4 no 3 pp 277ndash293 2006

[17] D Zhao and H Li ldquoShaking table tests and analyses of semi-active fuzzy control for structural seismic reduction with apiezoelectric variable-friction damperrdquo Smart Materials andStructures vol 19 no 10 Article ID 105031 2010

[18] W L He A K Agrawal and J N Yang ldquoNovel semiactivefriction controller for linear structures against earthquakesrdquoJournal of Structural Engineering vol 129 no 7 pp 941ndash9502003

[19] J N Yang and A K Agrawal ldquoSemi-active hybrid controlsystems for nonlinear buildings against near-field earthquakesrdquoEngineering Structures vol 24 no 3 pp 271ndash280 2002

[20] O E Ozbulut and S Hurlebaus ldquoOptimal design of supere-lastic-friction base isolators for seismic protection of highwaybridges against near-field earthquakesrdquo Earthquake Engineeringand Structural Dynamics vol 40 no 3 pp 273ndash291 2011

[21] D A Shook P N Roschke and O E Ozbulut ldquoSuperelasticsemi-active damping of a base-isolated structurerdquo StructuralControl and HealthMonitoring vol 15 no 5 pp 746ndash768 2008

[22] K D PhamG JinM K Sain B F Spencer Jr and S R LibertyldquoGeneralized linear quadratic Gaussian techniques for the windbenchmark problemrdquo Journal of Engineering Mechanics vol130 no 4 pp 466ndash470 2004

[23] S Nagarajaiah and S Narasimhan ldquoSmart base-isolated bench-mark building Part II Phase I sample controllers for linearisolation systemsrdquo Structural Control and Health Monitoringvol 13 no 2-3 pp 605ndash625 2006

Submit your manuscripts athttpwwwhindawicom

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

MathematicsJournal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Mathematical Problems in Engineering

Hindawi Publishing Corporationhttpwwwhindawicom

Differential EquationsInternational Journal of

Volume 2014

Applied MathematicsJournal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Probability and StatisticsHindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Journal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Mathematical PhysicsAdvances in

Complex AnalysisJournal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

OptimizationJournal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

CombinatoricsHindawi Publishing Corporationhttpwwwhindawicom Volume 2014

International Journal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Operations ResearchAdvances in

Journal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Function Spaces

Abstract and Applied AnalysisHindawi Publishing Corporationhttpwwwhindawicom Volume 2014

International Journal of Mathematics and Mathematical Sciences

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

The Scientific World JournalHindawi Publishing Corporation httpwwwhindawicom Volume 2014

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Algebra

Discrete Dynamics in Nature and Society

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Decision SciencesAdvances in

Discrete MathematicsJournal of

Hindawi Publishing Corporationhttpwwwhindawicom

Volume 2014 Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Stochastic AnalysisInternational Journal of

16 Mathematical Problems in Engineering

1 2 3 4 5 6 7 8 903

04

05

06

07

08

Excitation casePassive

GHFLC Optimal

1 2 3 4 5 6 7 8 907

08

09

10

11

12

13

14

15

Excitation case

Passive

GHFLC Optimal

J 3 J 5Figure 18 Comparisons on the performance indexes J

3and J5for different control cases (120575 = 4)

1 2 3 4 5 6 7 8 903

04

05

06

07

08

Excitation casePassive

GHFLC Optimal

1 2 3 4 5 6 7 8 907

08

09

10

11

12

13

14

15

Excitation casePassive

GHFLC Optimal

J 3 J 5

Figure 19 Comparisons on the performance indexes J3and J5for different control cases (120575 = 6)

Acknowledgments

This research was supported by National Natural ScienceFoundation of China under Grant no 51308487 no 41402261and no 51408526 Hebei Provincial Natural Science Founda-tion ofChina underGrant no E2014203055 and the ExcellentYouth Foundation of Hebei Educational Committee underGrant no YQ2013015 The support for this research is greatlyappreciated

References

[1] C Alhan and H Gavin ldquoA parametric study of linear and non-linear passively damped seismic isolation systems for buildingsrdquoEngineering Structures vol 26 no 4 pp 485ndash497 2004

[2] R S Jangid and J M Kelly ldquoBase isolation for near-faultmotionsrdquoEarthquake Engineering and Structural Dynamics vol30 no 5 pp 691ndash707 2001

[3] J Shen M-H Tsai K-C Chang and G C Lee ldquoPerformanceof a seismically isolated bridge under near-fault earthquake

Mathematical Problems in Engineering 17

ground motionsrdquo Journal of Structural Engineering vol 130 no6 pp 861ndash868 2004

[4] F Mazza A Vulcano and M Mazza ldquoNonlinear dynamicresponse of RC buildings with different base Isolation systemssubjected to horizontal and vertical components of near-faultground motionsrdquo Open Construction and Building TechnologyJournal vol 6 pp 373ndash383 2012

[5] F Mazza and A Vulcano ldquoEffects of near-fault ground motionson the nonlinear dynamic response of base-isolated rc framedbuildingsrdquo Earthquake Engineering and Structural Dynamicsvol 41 no 2 pp 211ndash232 2012

[6] O E Ozbulut and S Hurlebaus ldquoFuzzy control of piezoelectricfriction dampers for seismic protection of smart base isolatedbuildingsrdquo Bulletin of Earthquake Engineering vol 8 no 6 pp1435ndash1455 2010

[7] O E Ozbulut M Bitaraf and S Hurlebaus ldquoAdaptive controlof base-isolated structures against near-field earthquakes usingvariable friction dampersrdquo Engineering Structures vol 33 no12 pp 3143ndash3154 2011

[8] J M Kelly ldquoThe role of damping in seismic isolationrdquo Earth-quake Engineering and Structural Dynamics vol 28 no 1 pp3ndash20 1999

[9] F Mazza and A Vulcano ldquoNonlinear response of RC framedbuildings with isolation and supplemental damping at the basesubjected to near-fault earthquakesrdquo Journal of EarthquakeEngineering vol 13 no 5 pp 690ndash715 2009

[10] M Bitaraf and S Hurlebaus ldquoSemi-active adaptive control ofseismically excited 20-story nonlinear buildingrdquo EngineeringStructures vol 56 no 11 pp 2107ndash2118 2013

[11] D Das T K Datta and A Madan ldquoSemiactive fuzzy controlof the seismic response of building frames with MR dampersrdquoEarthquake Engineering and Structural Dynamics vol 41 no 1pp 99ndash118 2012

[12] A-P Wang and C-D Lee ldquoFuzzy sliding mode control for abuilding structure based on genetic algorithmsrdquo EarthquakeEngineering and Structural Dynamics vol 31 no 4 pp 881ndash8952002

[13] D G Reigles and M D Symans ldquoSupervisory fuzzy controlof a base-isolated benchmark building utilizing a neuro-fuzzymodel of controllable fluid viscous dampersrdquo Structural Controland Health Monitoring vol 13 no 2-3 pp 724ndash747 2006

[14] H-S Kim and P N Roschke ldquoGA-fuzzy control of smartbase isolated benchmark building using supervisory controltechniquerdquo Advances in Engineering Software vol 38 no 7 pp453ndash465 2007

[15] D Yang and Y Zhao ldquoEffects of rupture forward directivity andfling step of near-fault groundmotions on seismic performanceof base-isolated building structurerdquo Acta Seismologica Sinicavol 32 no 5 pp 579ndash587 2010

[16] Y E-A Mohamedzein J A Abdalla and A Abdelwahab ldquoSiteresponse and earthquake design spectra for central KhartoumSudanrdquoBulletin of Earthquake Engineering vol 4 no 3 pp 277ndash293 2006

[17] D Zhao and H Li ldquoShaking table tests and analyses of semi-active fuzzy control for structural seismic reduction with apiezoelectric variable-friction damperrdquo Smart Materials andStructures vol 19 no 10 Article ID 105031 2010

[18] W L He A K Agrawal and J N Yang ldquoNovel semiactivefriction controller for linear structures against earthquakesrdquoJournal of Structural Engineering vol 129 no 7 pp 941ndash9502003

[19] J N Yang and A K Agrawal ldquoSemi-active hybrid controlsystems for nonlinear buildings against near-field earthquakesrdquoEngineering Structures vol 24 no 3 pp 271ndash280 2002

[20] O E Ozbulut and S Hurlebaus ldquoOptimal design of supere-lastic-friction base isolators for seismic protection of highwaybridges against near-field earthquakesrdquo Earthquake Engineeringand Structural Dynamics vol 40 no 3 pp 273ndash291 2011

[21] D A Shook P N Roschke and O E Ozbulut ldquoSuperelasticsemi-active damping of a base-isolated structurerdquo StructuralControl and HealthMonitoring vol 15 no 5 pp 746ndash768 2008

[22] K D PhamG JinM K Sain B F Spencer Jr and S R LibertyldquoGeneralized linear quadratic Gaussian techniques for the windbenchmark problemrdquo Journal of Engineering Mechanics vol130 no 4 pp 466ndash470 2004

[23] S Nagarajaiah and S Narasimhan ldquoSmart base-isolated bench-mark building Part II Phase I sample controllers for linearisolation systemsrdquo Structural Control and Health Monitoringvol 13 no 2-3 pp 605ndash625 2006

Submit your manuscripts athttpwwwhindawicom

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

MathematicsJournal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Mathematical Problems in Engineering

Hindawi Publishing Corporationhttpwwwhindawicom

Differential EquationsInternational Journal of

Volume 2014

Applied MathematicsJournal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Probability and StatisticsHindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Journal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Mathematical PhysicsAdvances in

Complex AnalysisJournal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

OptimizationJournal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

CombinatoricsHindawi Publishing Corporationhttpwwwhindawicom Volume 2014

International Journal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Operations ResearchAdvances in

Journal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Function Spaces

Abstract and Applied AnalysisHindawi Publishing Corporationhttpwwwhindawicom Volume 2014

International Journal of Mathematics and Mathematical Sciences

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

The Scientific World JournalHindawi Publishing Corporation httpwwwhindawicom Volume 2014

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Algebra

Discrete Dynamics in Nature and Society

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Decision SciencesAdvances in

Discrete MathematicsJournal of

Hindawi Publishing Corporationhttpwwwhindawicom

Volume 2014 Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Stochastic AnalysisInternational Journal of

Mathematical Problems in Engineering 17

ground motionsrdquo Journal of Structural Engineering vol 130 no6 pp 861ndash868 2004

[4] F Mazza A Vulcano and M Mazza ldquoNonlinear dynamicresponse of RC buildings with different base Isolation systemssubjected to horizontal and vertical components of near-faultground motionsrdquo Open Construction and Building TechnologyJournal vol 6 pp 373ndash383 2012

[5] F Mazza and A Vulcano ldquoEffects of near-fault ground motionson the nonlinear dynamic response of base-isolated rc framedbuildingsrdquo Earthquake Engineering and Structural Dynamicsvol 41 no 2 pp 211ndash232 2012

[6] O E Ozbulut and S Hurlebaus ldquoFuzzy control of piezoelectricfriction dampers for seismic protection of smart base isolatedbuildingsrdquo Bulletin of Earthquake Engineering vol 8 no 6 pp1435ndash1455 2010

[7] O E Ozbulut M Bitaraf and S Hurlebaus ldquoAdaptive controlof base-isolated structures against near-field earthquakes usingvariable friction dampersrdquo Engineering Structures vol 33 no12 pp 3143ndash3154 2011

[8] J M Kelly ldquoThe role of damping in seismic isolationrdquo Earth-quake Engineering and Structural Dynamics vol 28 no 1 pp3ndash20 1999

[9] F Mazza and A Vulcano ldquoNonlinear response of RC framedbuildings with isolation and supplemental damping at the basesubjected to near-fault earthquakesrdquo Journal of EarthquakeEngineering vol 13 no 5 pp 690ndash715 2009

[10] M Bitaraf and S Hurlebaus ldquoSemi-active adaptive control ofseismically excited 20-story nonlinear buildingrdquo EngineeringStructures vol 56 no 11 pp 2107ndash2118 2013

[11] D Das T K Datta and A Madan ldquoSemiactive fuzzy controlof the seismic response of building frames with MR dampersrdquoEarthquake Engineering and Structural Dynamics vol 41 no 1pp 99ndash118 2012

[12] A-P Wang and C-D Lee ldquoFuzzy sliding mode control for abuilding structure based on genetic algorithmsrdquo EarthquakeEngineering and Structural Dynamics vol 31 no 4 pp 881ndash8952002

[13] D G Reigles and M D Symans ldquoSupervisory fuzzy controlof a base-isolated benchmark building utilizing a neuro-fuzzymodel of controllable fluid viscous dampersrdquo Structural Controland Health Monitoring vol 13 no 2-3 pp 724ndash747 2006

[14] H-S Kim and P N Roschke ldquoGA-fuzzy control of smartbase isolated benchmark building using supervisory controltechniquerdquo Advances in Engineering Software vol 38 no 7 pp453ndash465 2007

[15] D Yang and Y Zhao ldquoEffects of rupture forward directivity andfling step of near-fault groundmotions on seismic performanceof base-isolated building structurerdquo Acta Seismologica Sinicavol 32 no 5 pp 579ndash587 2010

[16] Y E-A Mohamedzein J A Abdalla and A Abdelwahab ldquoSiteresponse and earthquake design spectra for central KhartoumSudanrdquoBulletin of Earthquake Engineering vol 4 no 3 pp 277ndash293 2006

[17] D Zhao and H Li ldquoShaking table tests and analyses of semi-active fuzzy control for structural seismic reduction with apiezoelectric variable-friction damperrdquo Smart Materials andStructures vol 19 no 10 Article ID 105031 2010

[18] W L He A K Agrawal and J N Yang ldquoNovel semiactivefriction controller for linear structures against earthquakesrdquoJournal of Structural Engineering vol 129 no 7 pp 941ndash9502003

[19] J N Yang and A K Agrawal ldquoSemi-active hybrid controlsystems for nonlinear buildings against near-field earthquakesrdquoEngineering Structures vol 24 no 3 pp 271ndash280 2002

[20] O E Ozbulut and S Hurlebaus ldquoOptimal design of supere-lastic-friction base isolators for seismic protection of highwaybridges against near-field earthquakesrdquo Earthquake Engineeringand Structural Dynamics vol 40 no 3 pp 273ndash291 2011

[21] D A Shook P N Roschke and O E Ozbulut ldquoSuperelasticsemi-active damping of a base-isolated structurerdquo StructuralControl and HealthMonitoring vol 15 no 5 pp 746ndash768 2008

[22] K D PhamG JinM K Sain B F Spencer Jr and S R LibertyldquoGeneralized linear quadratic Gaussian techniques for the windbenchmark problemrdquo Journal of Engineering Mechanics vol130 no 4 pp 466ndash470 2004

[23] S Nagarajaiah and S Narasimhan ldquoSmart base-isolated bench-mark building Part II Phase I sample controllers for linearisolation systemsrdquo Structural Control and Health Monitoringvol 13 no 2-3 pp 605ndash625 2006

Submit your manuscripts athttpwwwhindawicom

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

MathematicsJournal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Mathematical Problems in Engineering

Hindawi Publishing Corporationhttpwwwhindawicom

Differential EquationsInternational Journal of

Volume 2014

Applied MathematicsJournal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Probability and StatisticsHindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Journal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Mathematical PhysicsAdvances in

Complex AnalysisJournal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

OptimizationJournal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

CombinatoricsHindawi Publishing Corporationhttpwwwhindawicom Volume 2014

International Journal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Operations ResearchAdvances in

Journal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Function Spaces

Abstract and Applied AnalysisHindawi Publishing Corporationhttpwwwhindawicom Volume 2014

International Journal of Mathematics and Mathematical Sciences

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

The Scientific World JournalHindawi Publishing Corporation httpwwwhindawicom Volume 2014

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Algebra

Discrete Dynamics in Nature and Society

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Decision SciencesAdvances in

Discrete MathematicsJournal of

Hindawi Publishing Corporationhttpwwwhindawicom

Volume 2014 Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Stochastic AnalysisInternational Journal of

Submit your manuscripts athttpwwwhindawicom

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

MathematicsJournal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Mathematical Problems in Engineering

Hindawi Publishing Corporationhttpwwwhindawicom

Differential EquationsInternational Journal of

Volume 2014

Applied MathematicsJournal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Probability and StatisticsHindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Journal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Mathematical PhysicsAdvances in

Complex AnalysisJournal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

OptimizationJournal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

CombinatoricsHindawi Publishing Corporationhttpwwwhindawicom Volume 2014

International Journal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Operations ResearchAdvances in

Journal of

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Function Spaces

Abstract and Applied AnalysisHindawi Publishing Corporationhttpwwwhindawicom Volume 2014

International Journal of Mathematics and Mathematical Sciences

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

The Scientific World JournalHindawi Publishing Corporation httpwwwhindawicom Volume 2014

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Algebra

Discrete Dynamics in Nature and Society

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Decision SciencesAdvances in

Discrete MathematicsJournal of

Hindawi Publishing Corporationhttpwwwhindawicom

Volume 2014 Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014

Stochastic AnalysisInternational Journal of


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