MIT LL Group 105 MQP Final Presentation · MIT LL Group 105 MQP Final Presentation This work is...

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David Kelly WPI-MIT Lincoln Laboratory 10/14/2015 Design of a Ku-Band Instrumentation Synthetic Aperture Radar System MIT LL Group 105 MQP Final Presentation This work is sponsored by the Department of the Air Force under Air Force Contract #FA8721-05-C-0002. Opinions, interpretations, recommendations and conclusions are those of the authors and are not necessarily endorsed by the United States Government. Approved for public release

Transcript of MIT LL Group 105 MQP Final Presentation · MIT LL Group 105 MQP Final Presentation This work is...

Page 1: MIT LL Group 105 MQP Final Presentation · MIT LL Group 105 MQP Final Presentation This work is sponsored by the Department of the Air Force under Air Force Contract #FA8721-05-C-0002.

David Kelly

WPI-MIT Lincoln Laboratory

10/14/2015

Design of a Ku-Band Instrumentation

Synthetic Aperture Radar System

MIT LL Group 105 MQP Final Presentation

This work is sponsored by the Department of the Air Force under Air Force Contract #FA8721-05-C-0002. Opinions, interpretations, recommendations

and conclusions are those of the authors and are not necessarily endorsed by the United States Government. Approved for public release

Page 2: MIT LL Group 105 MQP Final Presentation · MIT LL Group 105 MQP Final Presentation This work is sponsored by the Department of the Air Force under Air Force Contract #FA8721-05-C-0002.

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Outline

• Project Description

• Design

• Lab Test Results

• Field Test Results

• Conclusion

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MIT Lincoln Laboratory has developed a small form factor Ku-band Synthetic Aperture

Radar (SAR) intended for deployment on a Tier-1 UAV

Project Motivation

Example SAR Image

https://engineering.purdue.edu/~ace/sar/libcong.jpg

Pro: Small form factor great for field use on UAVs

Con: Performance sacrificed for a small form factor, not good as an

instrumentation radar

Goal: Design a chassis based radar system that is not limited by size, weight, or

power

37 cubic

inches

Page 4: MIT LL Group 105 MQP Final Presentation · MIT LL Group 105 MQP Final Presentation This work is sponsored by the Department of the Air Force under Air Force Contract #FA8721-05-C-0002.

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LL LiTE SAR MQP radar

Operating Frequency 16 to 17 GHz 16 to 17 GHz

Usable Instantaneous

Bandwidth 500 MHz 1 GHz

SAR Resolution 12” 6”

point-scatter side

lobes -20 dB -30 dB

Recording Mechanism Compact Flash 1 GbE Streaming

Real-time Display No Yes

Nominal Range 700 feet 700 feet

Range Swath 200 feet 200 feet

NEσ0 (SAR Sensitivity) -40 dB -40 dB

Radar Requirements

*The relationship of basic radar parameters to performance

can be obtained in open literature and textbooks such as:

Introduction to Radar Systems (Skolnik 1981)

Page 5: MIT LL Group 105 MQP Final Presentation · MIT LL Group 105 MQP Final Presentation This work is sponsored by the Department of the Air Force under Air Force Contract #FA8721-05-C-0002.

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Outline

• Project Description

• Design

• Lab Test Results

• Field Test Results

• Conclusion

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Frequency Modulated Continuous Wave (FMCW) Radar

TX

RX TX-RX

Basic Concept

FMCW Signal

Time (us) Time (us)

FMCW Output

Fre

qu

en

cy (

Hz)

Fre

qu

en

cy (

Hz)

Page 7: MIT LL Group 105 MQP Final Presentation · MIT LL Group 105 MQP Final Presentation This work is sponsored by the Department of the Air Force under Air Force Contract #FA8721-05-C-0002.

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Basic System Model

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Final Product

20in by 17.5in by 5in,

1750 cubic inches

Page 9: MIT LL Group 105 MQP Final Presentation · MIT LL Group 105 MQP Final Presentation This work is sponsored by the Department of the Air Force under Air Force Contract #FA8721-05-C-0002.

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Outline

• Project Description

• Design

• Lab Test Results

• Field Test Results

• Conclusion

Page 10: MIT LL Group 105 MQP Final Presentation · MIT LL Group 105 MQP Final Presentation This work is sponsored by the Department of the Air Force under Air Force Contract #FA8721-05-C-0002.

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• Measured the signal out of the Power Amplifier with a 60 Gsps Oscilloscope

• Frequency range of the signal was 16-17 GHz

• Signal was attenuated with a high power attenuator

• Waveform was saved with the Oscilloscope and analyzed in Matlab

Setup

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Spectrogram

• Useable Bandwidth of the Signal Measured to be 1.0923 GHz

• Noise cause by DAC spurs that can be removed with future work

Fre

qu

en

cy (

GH

z)

Po

wer

(dB

)

Time (us)

Page 12: MIT LL Group 105 MQP Final Presentation · MIT LL Group 105 MQP Final Presentation This work is sponsored by the Department of the Air Force under Air Force Contract #FA8721-05-C-0002.

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Range Profile and Spectrogram

-25dB

-18dB

-20dB

Range Profile

Fourier Range Cells

Po

wer

(dB

)

Existing Radar (1 GHz)

Existing Radar (500 MHz)

New Radar (1 GHz)

*Values are approximated

Page 13: MIT LL Group 105 MQP Final Presentation · MIT LL Group 105 MQP Final Presentation This work is sponsored by the Department of the Air Force under Air Force Contract #FA8721-05-C-0002.

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Outline

• Project Description

• Design

• Lab Test Results

• Field Test Results

• Conclusion

Page 14: MIT LL Group 105 MQP Final Presentation · MIT LL Group 105 MQP Final Presentation This work is sponsored by the Department of the Air Force under Air Force Contract #FA8721-05-C-0002.

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Test Setup

• Radar placed on top of parking

garage

• Targeted Bestic Dr between

Hartwell Ave and Schilling Cir

• Radar system used 15 dBi

antennas

• Target was a corner reflector

with an RCS = 34dBsm

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Moving Car

Stationary Objects

Corner Reflector Attached to a Car

Range (m)

Rd

ot

(m/s

)

Po

wer

(dB

)

Range-Velocity Map

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Intermod Anomaly

Intermodulation signals caused by frayed cables and a bad variable gain amplifier.

Range-Velocity Map Range-Velocity Map

Range (m) Range (m)

Po

wer

(dB

)

Po

wer

(dB

)

Rd

ot

(m/s

)

Rd

ot

(m/s

)

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Retest with New Amplifier and Cables R

do

t (m

/s)

Po

wer

(dB

)

Range (m)

Range-Velocity Map

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Field Measured Range Sidelobes

Range Sidelobe values of about -35dB , 10dB lower than measured in the lab

1 GHz bandwidth and

40 dB Taylor sidelobe

control used

-30dB

Range (m)

Range-Velocity Map

Po

wer

(dB

)

*Values are approximated

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Semi Truck Car

Corner Reflector

UPS Truck

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ISAR Image

Po

wer

(dB

)

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Keystone Transform on an ISAR Image

Rd

ot

(m/s

)

Po

wer

(dB

)

Range (m)

Range-Velocity Map

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Outline

• Project Description

• Design

• Lab Test Results

• Field Test Results

• Conclusion

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LL LiTE SAR MQP radar

How the

Parameter was

Measured

Operating Frequency 16 to 17 GHz 16 to 17 GHz Lab Oscilloscope

Usable Instantaneous

Bandwidth 500 MHz 1 GHz Lab Oscilloscope

SAR Resolution 12” 5” Calculated

point-scatter side

lobes -20 dB -35 dB Field Data

Recording Mechanism Compact Flash 1 GbE Streaming n/a

Real-time Display No Possible n/a

Nominal Range 700 feet 700 feet Field Data

Range Swath 200 feet 200 feet Field Data

NEσ0 (SAR Sensitivity) -40 dB -40 dB Calculated

Comparing the Radar Systems

*Values are approximated

Page 24: MIT LL Group 105 MQP Final Presentation · MIT LL Group 105 MQP Final Presentation This work is sponsored by the Department of the Air Force under Air Force Contract #FA8721-05-C-0002.

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• Remove DAC spurs with post processing or equalization

• Add isolators and check mixer power levels to remove unwanted signals

• Test with a more powerful laptop for more real time data

• Adapt the design for a Ka-band instrumentation radar system

• Test SAR capabilities of radar

Future Work

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Project Supervisor

– Andy Messier – Group 105

Initial Learning and Setup

– Jeffery Blanco – Group 105

– Tasadduq Hussain – Group 105

Hardware Debugging

– Ricky Hardy – Group 105

Field Testing

– Will Bartlett – Group 107

– Dennis Blejer – Group 105

Matlab Analysis

– Gerald Benitz – Group 105

Acknowledgements

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Supplemental Slides

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Bandwidth Issues of the Old Radar System

• Old radar used two analog waveform

generators

• One would start an LMF chirp when

the other finished it’s chirp

• When the two signals overlapped,

the filters in the radar could not

remove the resulting peaks

• Only about half of the bandwidth

could be used

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Pulse Width and SAR Resolution

Time Delay: 2 ∗𝑑

𝑐= 2 ∗

707 ∗.3048 𝑚

3∗108𝑚/𝑠= 1.437𝑢𝑠

Pulse Slope: 𝑓

𝑡𝑑𝑒𝑙𝑎𝑦=

0.014𝐺𝐻𝑧

1.437𝑢𝑠= 9.74𝑀𝐻𝑧 𝑝𝑒𝑟 𝑢𝑠

Pulse Width: ∆𝑓

𝑚𝑝𝑢𝑙𝑠𝑒=

17.3𝐺𝐻𝑧−16.2𝐺𝐻𝑧

9.74𝑀𝐻𝑧 𝑝𝑒𝑟 𝑢𝑠= 112.82𝑢𝑠

SAR Resolution: 𝑐

2𝐵=

3𝑒8

2(1.0923𝑒9)= 0.137𝑚 = 0.450𝑓𝑡