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Linear System Theory - Introduction to Simulink Prof. Robert X. Gao Electromechanical Systems Laboratory Department of Mechanical Engineering ME3253-01
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Linear System Theory - Introduction to Simulink

Prof. Robert X. GaoElectromechanical Systems LaboratoryDepartment of Mechanical Engineering

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Outline

Block Diagram Introduction Launching Simulink Modeling Procedure System Modeling with Simulink - Example Summary Practice

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Block Diagram

Definition: – A block diagram is an interconnection of blocks representing basic

mathematical operations in such a way that the overall diagram is equivalent to the system’s mathematical model.

Components: – Summer – Addition and subtraction– Gain – Multiplication– Integrator – Integration – Constant – No Input, Output Never Changes

Base: – Input – Output Equation– State – Variable Equations

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An Example of Block Diagram

For the given system,

Block Diagram

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Introduction

Definition: – “Simulink is a software package that enables you to model, simulate, and analyze

systems whose outputs change over time. ” - Mathworks

Features: – Model – based Design– Graphical Programming

Icon - Driven Build Systems by Drawing Block Diagrams

Applications:– Aerospace and Defense– Automotive – Communications – Electronics and Signal Processing– Medical Instrumentation– Etc.

Example – Plane Take - Off

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Launching Simulink

Launch MATLAB and Specify Work Directory

Launch SimulinkType “simulink” in command window Click Start Simulink Library Browser

Select Library

Block Description

Select Block

Block Search

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Modeling Procedure

Defining the Problem

Identifying System Components

Modeling System with Equations

Building the Simulink Block Diagrams

Running the Simulation

Validating the Simulation Results

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OUTSIDE SIMULINK

MODELING IN SIMULINK

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Example 4.7

A Parachute Jumper and a Mechanical Model

Conditions: – t = 0 as the moment the parachute opens– Risers fully extended, no deformation– Velocity: vj = 20 m/s, vp = 20 m/s– Constant = 9.807 m/s^2

Mass of the Parachute Mp 10 kG

Mass of the Jumper Mj 60 kG

Drag Coefficient of Parachute Bp 100 N/(m/s)

Drag Coefficient of Jumper Bj 10 N/(m/s)

Spring Constant of Riser KR 400 N/m

Values:

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Free – body Diagrams

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Equilibrium Equations

Equilibrium Equations

Re – write

( )

( )p p p p R j p p

j j j j R j p j

M x B x K x x M g

M x B x K x x M g

1 [ ( ) ]

1 [ ( ) ]

p p p R j p pp

j j j R j p jj

x B x K x x M gM

x B x K x x M gM

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Start a New Model

From the Library Browser, File New Model

Launch the Programming Interface

Drag Block Components From Library into This Area

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Programming

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Modeling of Parachute

1 [ ( ) ]p p p R j p pp

x B x K x x M gM

px px

px

( )j px x

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Modeling of Jumper

1 [ ( ) ]j j j R j p jj

x B x K x x M gM

( )j px x

jxjx

jx

Time

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Output Ports Assignment

Sequence Variable

1 Displacement of Parachute

2 Velocity of Parachute

3 Acceleration of Parachute

4 Displacement of Jumper

5 Velocity of Jumper

6 Acceleration of Jumper

7 Spring Elongation

8 Time

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Run the Simulation

Script

Run the Script (F5)

% DEMONSTRATION OF EXAMPLE 4.7 PARACHUTE

% 1. Value AssignmentMp = 10; % mass of parachute 10 kGMj = 60; % mass of jumper 60 kGBp = 100; % drag coef. of parachute 100 N/(m/s)Bj = 10; % drag coef. of jumper 10 N/(m/s)KR = 400; % spring constant of riser 400 N/m

% 2. Simulation Executionsim('parachute');

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Simulation Result

Workspace

Output Variables

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Visualization of Result % PLOT THE SIMULATION RESULT

% OUTPUT VARIABLE : yout % TIME OUTPUT: toutfigure; subplot(4,1,1); % 1ST PLOTplot(tout,yout(:,1),'b','LineWidth',3); % PLOT DISP. OF PARACHUTE VS. TIMEhold on;grid on;plot(tout,yout(:,4),'--r','LineWidth',3); % PLOT DISP. OF JUMPER VS. TIMEylabel('meter','FontSize',22); % SET YLABLE set(gca,'FontSize',16); % SET FONT SIZE OF AXES

subplot(4,1,2); % 2ND PLOTplot(tout,yout(:,2),'b','LineWidth',3); % PLOT VELOCITY OF PARACHUTE VS. TIMEhold on;grid on;plot(tout,yout(:,5),'--r','LineWidth',3); % PLOT VELOCITY OF JUMPER VS. TIMEylabel('meter/sec.','FontSize',22); % SET YLABLE set(gca,'FontSize',16); % SET FONT SIZE OF AXES

subplot(4,1,3); % 3RD PLOTplot(tout,yout(:,3),'b','LineWidth',3); % PLOT ACCELERATION OF PARACHUTE VS. TIMEhold on;grid on;plot(tout,yout(:,6),'--r','LineWidth',3); % PLOT ACCELERATION OF JUMPER VS. TIMEylabel('meter/sec.^2','FontSize',22); % SET YLABLE set(gca,'FontSize',16); % SET FONT SIZE OF AXES

subplot(4,1,4); % 4TH PLOTplot(tout,yout(:,7),'k','LineWidth',3); % PLOT ELONGATIONylabel('meter','FontSize',22); % SET YLABLE xlabel('Time/sec.','FontSize',22); % SET XLABLEset(gca,'FontSize',16); % SET FONT SIZE OF AXESgrid on;

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Plot

0 0.5 1 1.5 2 2.5 3 3.5 40

20

40

met

er

0 0.5 1 1.5 2 2.5 3 3.5 40

10

20

30

met

er/s

ec.

0 0.5 1 1.5 2 2.5 3 3.5 4-200

-100

0

100

met

er/s

ec.2

0 0.5 1 1.5 2 2.5 3 3.5 40

2

4

met

er/s

ec.2

Time/sec.

Elongation

ParachuteJumper

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Summary

Introduction to Block Diagram

Introduction to Simulink

Demonstration of Model – based Design

Demonstration of Simulink Operation

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Practice

Launch MATLAB

Get Familiar with Matrix Operations

Try to Solve a Simple Problem with MATLAB

Try to Solve a Simple Problem with Simulink

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