SLIDE 1
Nanyang Research Programme Presentation EEE19: Beautiful Arrays Kwa - - PowerPoint PPT Presentation
Nanyang Research Programme Presentation EEE19: Beautiful Arrays Kwa - - PowerPoint PPT Presentation
Nanyang Research Programme Presentation EEE19: Beautiful Arrays Kwa Shi Min Hwa Chong Institution (College Section) INTRODUCTION AIMS METHODOLOGY RESULTS AND DISCUSSION CONCLUSION INTRODUCTION Example: Satellite Communication Satellites
SLIDE 2
SLIDE 3
Example: Satellite Communication
Satellites using same frequency bands Interference with another satellite! Target satellite Antenna with low directivity Antenna with high directivity
INTRODUCTION
SLIDE 4
INTRODUCTION
Background: Antenna Array Directivity
- Major uses in radar, sonar, wireless telecommunication, etc.
- Radiate power in a specific direction
- Single-element antenna usually limited in directivity
- Antenna array synthesis
1. Array weight - costly in implementation 2. Array geometry
- Current analytical, numerical and algorithmic approaches have yet to
reveal a general theory for non-uniform arrays
SLIDE 5
INTRODUCTION
Approach: Beautiful Antenna Array Geometry
- Implement symmetry, golden ratio (GR) and silver ratio (SR) in the
determination of inter-element spacings of non-uniform arrays
- Led to many new theories when used in other fields
- GR used implicitly before in phased arrays research – used
solely as a special logarithmic spiral array
- Not explicitly studied in the design of arrays in a general
sense
SLIDE 6
AIMS
1 2
Investigate effect of beautiful antenna array geometry on antenna array directivity Increase antenna array directivity to higher than that
- f control using beautiful antenna array geometry
SLIDE 7
METHODOLOGY
Geometry Design
- Design schemes for testing
- Adapt for linear and planar arrays
- Design tests to investigate effects
1
SLIDE 8
METHODOLOGY
Scheme 1: Scheme 2:
SLIDE 9
METHODOLOGY
Scheme 3: Scheme 4:
SLIDE 10
METHODOLOGY
Scheme 0: Linear Control Array
SLIDE 11
METHODOLOGY
Geometry Design
- Design schemes for testing
- Adapt for linear and planar arrays
- Design tests to investigate effects
1
SLIDE 12
METHODOLOGY
SLIDE 13
Planar Control Array
METHODOLOGY
SLIDE 14
METHODOLOGY
Geometry Design
- Design schemes for testing
- Adapt for linear and planar arrays
- Design tests to investigate effects
1
SLIDE 15
METHODOLOGY
Geometry Design
- Design schemes for testing
- Adapt for linear and planar arrays
- Design tests to investigate effects
1
Control parameters 1. Array weights 2. Frequency 3. Wavelength Variable 1. Element position vectors
SLIDE 16
Beampattern Generation
- Real world antenna simulated by computer-programmed isotropic elements
- Plot of array response to a plane-wave front
- with unity amplitude arriving in direction (θ, φ)
- A function of elevation angle (θ), azimuth angle (φ) &
element position vectors (r)
rn(xn, yn, zn)
xn zn yn
Direction of Source
φ θ
Plane-Wave Front
y x x(t) sampled signals at outputs of sensor elements w1 uniform weights y(t) array output
METHODOLOGY
2
x1(t) xL(t) x2(t) w1 w1 w1 y(t)
SLIDE 17
Performance Measurement
- Observe and record Main Beamwidth, Mainlobe Gain and Peak Sidelobe
Gain
- Narrow Main Beamwidth
Low Sidelobe Level (SLL) High Directivity
METHODOLOGY
3
11-Element Symmetric GR Scheme 4 Root Value 0.587 Uniform Linear Array Main Beamwidth Mainlobe Peak Sidelobe
Gain (abs) Azimuth Angle (⁰)
SLIDE 18
RESULTS AND DISCUSSION
- Length increase, main beamwidth decrease
- Coincides with general theory of uniformly-spaced linear
arrays – for the same number of elements, the larger aperture will have a smaller beamwidth
- Presence of undesirable spacings of (<0.5 or
>1 wavelength), SLL increase
- Dense regions reduce the elements contribution to the
directivity since they are too close in terms of wavelength, while empty regions increase the under-sampling
Preliminary Testing
RESULTS AND DISCUSSION (LINEAR ARRAY)
SLIDE 19
Effect of Reflection Symmetry
RESULTS AND DISCUSSION (LINEAR ARRAY)
SLIDE 20
- 20.00
- 10.00
0.00 Scheme 1 Scheme 2 Scheme 3 Scheme 4 SLL (dB) Scheme Asymmetric Symmetric
* Effect of Reflection Symmetry
RESULTS AND DISCUSSION (LINEAR ARRAY)
SLIDE 21
RESULTS AND DISCUSSION
Effect of Symmetry vs GR Schemes
RESULTS AND DISCUSSION (LINEAR ARRAY)
SLIDE 22
RESULTS AND DISCUSSION Scheme> Symmetry
Effect of Symmetry vs GR Schemes
Scheme 1 Scheme 2 Scheme 3 Scheme 4
- 20.00
- 10.00
0.00 Scheme 3 Scheme 4 Scheme 1 SLL (dB) Scheme
RESULTS AND DISCUSSION (LINEAR ARRAY)
SLIDE 23
Let the distances between origin and X number of elements in a scheme be s1, s2, …, sx. E.g. When the scheme is subjected to a root value of 0.1, the distances will become s1
0.1, s2 0.1, …, sx 0.1.
- To obtain optimized power and best scheme
- Reduce side lobe amplitudes and grating lobes
RESULTS AND DISCUSSION (LINEAR ARRAY)
Effect of GR with Change in Root Value
SLIDE 24
RESULTS AND DISCUSSION
- 10.00
- 5.00
0.00
0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0 Root Value Scheme 0 Scheme 1 Scheme 2 Scheme 3 Scheme 4
Larger root values forces inter- element spacings to become more similar→oscillation
Effect of GR with Change in Root Value
Further test portions to 3s.f.
Consider main beamwidth when SLLs are similar SLL (dB)
RESULTS AND DISCUSSION (LINEAR ARRAY)
SLIDE 25
RESULTS AND DISCUSSION
0.00 100.00 200.00 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1 Main Beamwidth (°) Root Value Scheme 0 Scheme 1 Scheme 2 Scheme 3 Scheme 4 .0
Effect of GR with Change in Root Value
RESULTS AND DISCUSSION (LINEAR ARRAY)
SLIDE 26
RESULTS AND DISCUSSION (LINEAR ARRAY)
Effect of GR with Change in Number of Elements
9 11
SLIDE 27
RESULTS AND DISCUSSION
+2 gradual
Effect of GR with Change in Number of Elements
- 18.00
- 13.00
- 8.00
3 5 7 9 11 13 15 17 19 SLL (dB) Number of Elements Scheme 0 Scheme 4
RESULTS AND DISCUSSION (LINEAR ARRAY)
SLIDE 28
RESULTS AND DISCUSSION
Main Beamwidth↓21% SLL↓28% Azimuth Angle (⁰)
11-Element Symmetric GR Scheme 4 Root Value 0.587 Uniform Linear Array Main Beamwidth Mainlobe Peak Sidelobe
Beampatterns of Finalised Symmetric GR Scheme vs Control
RESULTS AND DISCUSSION (LINEAR ARRAY)
Gain (abs)
SLIDE 29
Effect of Order of Rotational Symmetry
RESULTS AND DISCUSSION RESULTS AND DISCUSSION (PLANAR ARRAY)
Order 4 Order 8
SLIDE 30
Effect of Order of Rotational Symmetry
- 30.00
- 15.00
0.00 Scheme 0Scheme 2Scheme 3Scheme 4 SLL (dB) Scheme Order 4 Order 8
*
RESULTS AND DISCUSSION RESULTS AND DISCUSSION (PLANAR ARRAY)
SLIDE 31
- 30.00
- 15.00
0.00 20 30 40 50 60 70 80 90 100 SLL (dB) Number of Elements Scheme 0 Scheme 2 Scheme 3 Scheme 4
RESULTS AND DISCUSSION
but stagnates
RESULTS AND DISCUSSION (PLANAR ARRAY)
Effect of SR with Change in Number of Elements
SLIDE 32
Let the distances between origin and X number of elements in a scheme be s1, s2, …, sx.
- Eg. When the scheme is subjected to a scaling value of 1.1, the
distances will become 1.1 * s1, 1.1 * s2, …, 1.1 * sx.
- Optimize SLL and beamwidth
Effect of SR with Change in Scaling Value
RESULTS AND DISCUSSION (PLANAR ARRAY)
SLIDE 33
RESULTS AND DISCUSSION RESULTS AND DISCUSSION (PLANAR ARRAY)
Effect of SR with Change in Scaling Value
0.00 60.00 120.00 1.0 1.1 1.2 1.3 1.4 1.5 Main Beamwidth (°) Scaling Value Scaling Value (≥1)↑, Main Beamwidth↓ Control array has main beamwidth of 40.00⁰, therefore further tested to 2d.p. →1.25, 38.00⁰
SLIDE 34
RESULTS AND DISCUSSION (PLANAR ARRAY)
Effect of SR with Change in Scaling Value
Scaling Value (≥1)↑, SLL↓
- 30.00
- 15.00
0.00 1.0 1.1 1.2 1.3 1.4 1.5 SLL (dB) Scaling Value 1.25, -23.41dB
SLIDE 35
RESULTS AND DISCUSSION
Gain (dB)
RESULTS AND DISCUSSION (PLANAR ARRAY)
Cartesian Beampattern of Finalised Symmetric SR Scheme
SLIDE 36
Main Beamwidth↓5.0% SLL↓18% Elevation Angle (⁰) Gain (dB)
RESULTS AND DISCUSSION (PLANAR ARRAY)
Polar Beampattern of Finalised Symmetric SR Scheme
SLIDE 37
CONCLUSION
Novel empirical study on the effects of using symmetry, GR and SR in the design of non-uniform antenna arrays on the directivity of beampatterns
Beautiful Antenna Array Geometry: Potential Way of Increasing Antenna Array Directivity
1 2 Symmetry, GR and SR can be used to increase antenna array directivity Significant increase of antenna array directivity in comparison with control
SLIDE 38