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Contact: webmaster@fasant · 2015-07-10 · Chaff analyses. ISAR and RCS map. ... DOPPLER Tool for...

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Contact: [email protected] www.fasant.com
Transcript

Contact:

[email protected]

www.fasant.com

Index Introduction

Applications

Modules of NewFasant SW Suite

Monurbs Mesher Antenna Design Reflector Antenna Design Antenna Placement Electromagnetic Compatibility Impulse Response Patch Antenna Radar Cross Section (RCS)

GTD-Fasant Radio Propagation Antenna Placement Dynamic Scenarios

Pogcros

ISAR & RCS Map

Doppler

Infrared

Radome

Periodical Structures

Reflectarrays

Ultra-conformed Reflectors

Antenna Arrays

Circuit Analysis

Testing Capabilities

Companies, Institutes and Universities involved in projects

1. Introduction

• NEWFASANT S.L is an spin-off company of the Computational ElectromagneticGroup (ECG) of Alcalá University, SPAIN

• The GEC was born in 1990 and NEWFASANT was founded in 2010

• NEWFASANT development team is formed by:

• 16 Senior Engeeners (PhD. Degree)

• 12 Engeeners.

• GEC and NEWFASANT Projects:

• 60 International.

• 55 National.

• Publications:

• 80 Papers in Internationals Journal.

• 250 Communication in Symposium.

1. Introduction

NEWFASANT works in the fields of:

Analysis of antennas on board complex structures.

Design of antennas, radomes and FSS.

Design of MIMO antennas.

Study of the electromagnetic compatibility

Channel modelling and frequency planning in mobile communications.

Design of passive radio frequency components.

Scattering of electromagnetic waves with application to RCS of complex structures.

ISAR, RCS map, Radiation map, Doppler analyses.

Thermal analysis and infrared images.

Applications

Electronic Compatibility

Antenna: Analysis and Design

Antennas on-board complex structures

Radar Cross Section (RCS).

Chaff analyses.

ISAR and RCS map.

Doppler frequency shifts

Radio Propagation

Radio System Analysis

Design of Passive MicrowaveComponents.

Radomes: Analysis and Design

Reflectarrays: Analysis and Design

Ultraconformed Reflector

MIMO antennas

Frequency Selective Surfaces (FSS)

Infrared

2. Modules of NewFasant SW Suite

All the SW tools of NEWFASANT have been groupedin the computer simulation suit NEWFASANT.

NEWFASANT is composed by a series of modules thatshare a common user interface

NewFasant EM Application Suite (I)GTD GTD/UTD and PO tool for the analysis of on-board antennas

RADIO

PROPAGATIONGTD/UTD and PO tool for the analysis radio wave propagation in indoor and

outdoor scenarios.

MOMCROS MoM tool with MLFMA for RCS computations of complex bodies.

POGCROS PO/SPM tool for the computation of the RCS of complex bodies.

ISARTool for the computation of range profiles, ISAR and RCS reflectivity, using MoM or GO/PO.

DOPPLER Tool for the calculation of Doppler frequency shift using MoM or GO/PO.

CIRCUITSTool for the analysis and design of planar circuits, waveguide circuits and wire antenna arrays using MoM.

RADOME Tool for the analysis and design of radomes.

REFLECTARRAY Tool for the analysis and design of reflectarrays and subreflectarrays.

PERIODIC Tool for analysis and design of periodic structures and metamaterials.

MONURBS MoM tool with MLFMA for antenna analysis and design.

IR Tool for computing thermal analyses and infrared images.

NewFasant EM Application Suite (II)ULTRA-

CONFORMED

REFLECTORS

It provides the analysis and design of only-metallic reflectarrays or sub-

reflectarrays, in terms of reflectors obtained by conformation of smooth

surfaces. The designed antennas can be analyzed using either PO or a

full-wave MoM approach.

ARRAYSFor the replication of a primitive and use of specialized characteristic

basis functions in order to analyze efficiently large finite arrays using a MoM approach.

CHAFFThis module provides the analysis and design of chaff clouds using different element and cloud geometries.

NewFasant EM Application Suite (III)

MIMO

Design of MIMO antennas.

Analysis of MIMO antennas over an arbitrary

scene

MIMO

MEASUREMENT

Characterization of MIMO parameters by

means of an emulation of a reverberation

chamber for MIMO measurement

MONURBS Module MONURBS is a parallelized Moment Method computer tool for:

3D analysis of complex antennas, on board antennas, electromagnetic compatibility radar cross section (RCS).

This module is based on MLFMA(Multilevel Fast Multipole Algorithm) Preconditioners Macro basis functions (CBFs) Domain Decomposition Technique

Feature of our Mesher Pre-processing techniques

Topologies detection

Forcing electrical continuity

Accelerated paving algorithm

Quadrilateral elements with

Sporadic triangles (both surface fitted)

Parallelized code

Multilevel mode

Very fast meshings

Manual or Automatic

Feature of our Mesher Adaptative meshing

ANTENNA DESIGN (MONURBS Module) This module allows the efficient design of antennas and other structures

due to its parametric optimizer.

A large library of antenna primitives is available:

horns, patches, helices, Slot Vivaldi antennas, single and multiple reflectors, blades, coaxial feed antennas, spirals, arrays, etc.

The user can also build and optimize his own new antenna geometries.

ANTENNA DESIGN (MONURBS Module)

REFLECTOR ANTENNA DESIGN (MONURBS Module)

ANTENNA PLACEMENT (MONURBS Module)

VHF (1.6 GHz.)

X

YZ

GS (3.96 GHz.)

DME (12.9 GHz.)

Medidas PO MFIE-CGM#1

grados

)(dBES

grados

)(dBES

Analysis of antennas on board aircraft. VHF antenna. Frequency 1.6 GHz

Antenna on car

APPLICATION OF MONURBS TO A ESA EMC PROJECT

23

EFFECTIVE TECHNIQUE FOR SYSTEM LEVEL PREDICTION OF ELECTROMAGNETIC EMISSIONS FROM ELECTRONIC DEVICES

AND CABLES IN SATELLITES

ESA Project: “Effective alternative technique to radiated

system level verification”, TL-OF-075/2005. 2005-2006.

Results Published in IEEE Antennas & Propagation Magazine,

April 2010, pp 71 – 85

“A systematic approach for radiated system level verification of

unknown sources inside satellites from unit level measurements”.

F. Saez de Adana, M.F. Cátedra, J.M. Gómez, R. Mittra, J.

Berkowitsch, F. Gutiérrez, M. Alfonsea.

24

A technique for the prediction of the radiation of electronic cables and

devices at system level was developed.

The objective is to predict the emissions of the equipment inside the

satellite without the necessity of measurements inside the satellite.

Band: 100MHz-10GHz

25

Measurements in all the complete band were carried for validation

26

Validation

Case 4: Two interconnected boxes.

27

Validation

• Frequency 4000 MHz

Probe rail 1 Probe rail 2

30

35

40

45

50

55

60

65

70

1 11 21 31 41 51 61 71 81 91 101

Et MoM Et OA

Et (dBV/m)

Point

30

35

40

45

50

55

60

65

70

1 11 21 31 41 51 61 71 81 91 101

Et MoM Et OA

Et (dBV/m)

Point

28

Validation

• Mean error and standard deviation

Frequency Mean error Standard

deviation

300 MHz 0.233 dB 0.231 dB

1500 MHz 1.128 dB 0.868 dB

4000 MHz 2.603 dB 2.799 dB

7000 MHz 2.088 dB 2.372 dB

EMC analysis of Evektor’s EV55 Aircraft using MONURBS

29

•We have found many problems with the “clean model”

•We worked with the “full model” after repairing:

•Improved relocation of controls points

•Insuring continuity between surfaces

30

500 MHz

Full Model meshing 5 00 MHz, 50,982 elements

31

Current distribution, Full Model, 5 00 MHz, about 100,000 subdomains

MoM +MLFMM with preconditioner

32

Field intensities at internal point (5.4,0.,0.) from 250 MHz- to 500 MHz. Full Model

MoM+ MLFMM with preconditioner

33

Radiation field pattern, Full Model , 5 00 MHz, about 100,000 subdomains

MoM +MLFMM with preconditioner

Impulse response (MONURBS Module)

Impulse response studies,

frequency 1.5 GHz

Impulse response (MONURBS Module)

Impulse response studies,

frequency 1.5 GHz

Patch antenna (MONURBS Module)

Microstrip antenna onboard satellite

Patch antenna (MONURBS Module)

Microstrip antenna on board rocket

RADAR CROSS SECTION (MONURBS Module)

RCS analysis of reflector (ESA) (MONURBS Module)

Casagrain reflector

22 m m diameter, 5.3

GHz

RCS of cavities (MONURBS Module)

• The cavity is cylindrical,•with a depth of 4 m,•a radius of 1 m.•The fan is 0.8 m. from the cavity bottom.

• All the following results have been obtained for a freq. of 3GHz.•

•A laptop computer with a quad processor was used.

•The memory required in all the cases was lower than 6 GB,

•CPU-time for monostatic analysis, 15 min.

Cylinder with RAM in the left

FASANT - Module

FASANT is a very efficient computer tool for the 3D analysis of antennas onboard satellites, aircrafts and other complex bodies.

The kernel of the program is based on Geometrical Optics (GO), PhysicalOptics (PO) and Uniform Theory of Diffraction. A combination of the AngularZ-Buffer (AZB), the Volumetric Space Partitioning (SVP) and the A* heuristicalgorithm is applied for the ray-tracing acceleration.

Radio-Coverage Analysis (FASANT Module)

Radio-Coverage Analysis (FASANT Module)

Radio-Channel Analysis (FASANT Module)

FASANT also provides radio channel parameters:

impulse response, CDMA analysis, Power delay profiles, etc.

Antenna Placement (FASANT Module)

Study on antenna radiation pattern of antennas on board JASON 1 satelite

of CNES (FRANCE).

Frequency: 2.2 GHZ

Etheta

-60

-50

-40

-30

-20

-10

0

10

-180 -161 -142 -123 -104 -85 -66 -47 -28 -9 10 29 48 67 86 105 124 143 162

Cut phi=67.5º

dB

Measure

FASANT

CPU-time 5 minutos in a PCMemory; 200 MB de RAM

Radio-Channel Analysis (FASANT Module)

FASANT provides a new approachto analyze dynamic scenarios(some objects and/or antennas canhave translation and/or rotationmovements)

Radio-Channel Analysis (FASANT Module)

Static and dynamic results can be visualized:

POGCROS – Module

POGCROS (Physical Optic/Geometrical Optics Code for RadarCross Section Computation) is a parallelized, efficient, accurateand fast computer tool for the analysis of the Radar Cross Section(RCS) of electrically large complex targets.

With Speed-upTime: 5 s.Memory: 20 KB4 processors

Without Speed-upTime: 2 min.Memory: 20 KB4 processors

This case has been run in a Intel Core i7 with 8 GB RAM and 4

processors

RCS of Cavities (POGCROS Module) The objects can include Perfect Electric Conductor (PEC), dieletric or magnetic

materials or PEC covered by Radar Absorbing Materials (RAM). POGCROS can alsohandle the interaction of terrestrial or maritime targets with their surroundingenvironment

POGCROS (PO)

MONURBS(MoM)

POGCROS takes less than 1 min formonostatic analysis (91 directions).

ISAR – Module

ISAR (Inverse Synthetic Aperture Radar) is a parallelized, efficient,accurate and fast computer tool used to obtain ISAR images, RangeProfile images and RCS maps of electrically large complex targets.

Range Profile (ISAR Module)

ISAR Computation (ISAR Module)

• For 3 GHz. Satellite mockup 64 x 64 samples. 1 GHz Bandwidth

• Angular margin 6º

=90º and =0º

Satellite Mockup

RCS MAP (ISAR Module)RCS Map (MONURBS)

• Methods before can be applied to obtain RCS Scatter Map (Hot Spot)

• Obtain the most contributing parts to the RCS in an specific direction

HelIcopter =90º and =0º

HelIcopter =180º and =0º

Frequency 1.5 GHz

Current Distribution

RCS MAP (ISAR Module)

RCS Map (MONURBS)

Boeing =90º and =0º (MoM)

Boeing =90º and =0º (PO Iterative)

Frequency 1.5 GHz

DOPPLER – Module

DOPPLER is a parallelized, efficient, accurate and fast computertool used to obtain Doppler frequency spectrum of electricallylarge complex bodies.

RCS of Moving Target (DOPPLER Module)

The cavity is cylindrical, with a depth of 4m, a radius of 1m. The fan is 0.8mfrom the cavity bottom. All the following results have been obtained with theprevious cavity with a two-blade fan for a frequency of 3 GHz.

RCS of Moving Target (DOPPLER Module)

Doppler Spectrum obtained using POGCROS, monostatic case, Theta= 10,phi=90. The blades are rotating with an angular speed of 1000 rad/s. About 3seconds of CPU.

IR – Module

INFRARED is an accurate and fast computer tool for the infraredanalysis of arbitrary structures, such as ground vehicles, aircrafts,ships… The parameters of the thermal scenario and exhaust gasescan be easily modeled with the graphical user interface provided.

RADOME – Module

RADOME moduleRADOME is a parallelized accurate and fast computertool for the analysis of antenna with radomes, including multilayerradomes with embedded Frequency Selective surfaces (FSS). An iterativeMoM approach is used in the simulations. Optimization features for theradome design are also included. radomo 2.8 metros phi=90

-3.00E+01

-2.00E+01

-1.00E+01

0.00E+00

1.00E+01

2.00E+01

3.00E+01

4.00E+01

1 11 21 31 41 51 61 71 81 91 101 111 121131 141 151 161 171 181

RADOME landa6

NO RADOME SIMPLE

Radome 4mm

72

Radomes/LensesDielectric radome with FSS at 15 GHz

73

Radomes/Lenses

Dielectric radome with FSS at 15 GHz

PERIODICAL STRUCTURES – Module

PERIODICAL STRUCTURES is an efficient and accurate computer tool usedto obtain the reflection and transmission coefficients of single/multiplelayers applying the Moment Method, considering finite sized or infinitestructures. An optimizer feature addresses the design of periodical structures

REFLECTARRAY – Module

5 6 7 8 9

x 10-3

-200

-150

-100

-50

0

50

100

150

200

250

Re

fle

cte

d P

ha

se

(d

eg

)

External Length (m)

REFLECTARRAY addresses the analysis and design of reflectarrays. The usercan choose between several primitives for the design of periodic structures,or create new ones. The periodic structures can include one or more layers.The reflectarray surface can be arbitrarily shaped. This module provides thelayout of the quasi periodic structures ready to be machined.

REFLECTARRAY – Module

The designed antennas can be analyzed using either PO or a full-waveMoM approach

Three layers reflectoarray analysis (REFLECTARRAY Module)

Frequencies: 11.05 GHz and 12.1 GHz Polarization Dual

Dual Band Reflectoarray (REFLECTARRAY Module)

Frequencies: 12 and 14 GHz

81

Offset configuration to avoidblockage

Frequency = 16 GHzSize= 300x300 mmFocus = -148.5, 0, 228.6 mmCell period =9mmArray = 33x33 cells

Gain = 30,62dBiSteering : ϴ=10º, φ=0ºDual-layer cell.

Offset Reflectarray

82

Iterative proccess to obtain the phase distribution in the antenna aperture to conform the antenna beam to targeted shapes.

Antenna layout is obtained automatically (reflectarrays or ultra-conformed reflectors) for any satellite position.

Conformed beam obtention

Ultra-Conformed Reflectors• This antenna provides almost the same gain as the traditional

parabolic reflectors, while a small volume remains.

• It has a low profile and a low weight like reflectarrays.

• It has lower losses and it is easier to fabricate

• The design process is faster, because the design of microstripradiating elements is not required.

• The manufacturing process is simpler, due to it not needing any complex layout to scatter the incident field.

• The cost of making this flat reflector is comparable toconventionalreflectors and reflectarrays.

85

Parabolic shape

Frequency = 100 GHzSize, 60x60mmFocus = 0, 0, 60mmParabole Focus = 0, 0, 30mmSteering : ϴ=10º, φ=0ºGain = 33,3dBi

Parabolic Squared Ultra-Conformed Reflector

Antenna arrays

Array composed of 10x10 quadrifilar helixes to radiate with circular polarization.

Antenna arrays

Array composed of 20x20 conical horns fed to radiate with circular polarization.

CIRCUIT ANALYSIS – Module

Primitives for antennas and circuit components are available.Optimization tools are also available for the design of microstripcomponents, antennas and circuits

Hairpin Filter

CIRCUIT ANALYSIS – Module

CIRCUIT ANALYSIS is an accurate and fast computer tool for the analysis of S,Y and Z parameters of antennas and for the analysis of microstrip circuits andantennas.

3. Testing Capabilities

Automatic Measurements in near field (planar, cylindrical andspherical)

anechoic chamber form 0.5 up to 40 GHz (6mx4mx3.8m) All software (mechanical control, scanning and field translation

developed by us)

5. Companies, institutes and universities involved in projects

5. Companies, institutes and universities involved in projects

CONTACT ADRESS:

NEWFASANT S.L.Avenida de Buendia 11,

19005 Guadalajara, Spain

Email: [email protected]


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