Synthetic Aperture Radar Imager

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Synthetic Aperture Radar Imager Team 18 Spring 2016: Presentation I MEMBERS: LUKE BALDWIN JOSH DENNIS KAYLEN NOLLIE DESMOND PRESSEY SPONSOR: NORTHROP GRUMMAN CONTACT: MIKE BLUE ADVISOR: DR. DORR CAMPBELL INSTRUCTOR: DR. NIKHIL GUPTA DATE: 1/19/2016

Transcript of Synthetic Aperture Radar Imager

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Synthetic Aperture Radar Imager

Team 18Spring 2016: Presentation I

M E M B E R S :

L U K E B A L D W I N

J O S H D E N N I S

K AY L E N N O L L I E

D E S M O N D P R E S S E Y

S P O N S O R : N O R T H R O P G R U M M A N

C O N TA C T: M I K E B L U E

A D V I S O R : D R . D O R R C A M P B E L L

I N S T R U C TO R : D R . N I K H I L G U P TA

D AT E : 1 / 1 9 / 2 0 1 6

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Outline• Review of Project Scope

• Review Previous Progress

• Design Updates

• Procurement

• Schedule and Future Plans

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Working SAR

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[1]

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Imaging Radar Operational Concept40 x 40 inch scene

20 [ft] range to scene center

16 - 2.5 inch1-D Cells in Azimuth andElevation

5 x 5 feet20nS wide RFPulse @ 10 GHz

Antenna Array

Beams are formedDigitally with FourierTransform, 16 in AzimuthAnd 16 in Elevation

PC Display

VGA Connection

16 - Azimuth16 - Elevation

[4]

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Project GoalsCreate a Synthetic Aperture Radar:• Project Features:• Weapons detection for homeland security

• Stationary

• Low resolution

• Concealable

• Low Cost

• Relatively mobile

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Project Organization• ME Team• Structure

•Horn holders

• EE Team•Hardware Box

• Signal processing

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Second Generation Improvements• Mobility• Attach wheels

• Weight• < 80 lbs

• Horn Adjustment• Aligned within 1ft circle at 20ft away

• Stability• Movement causes artificial phase shift

• Max movement: 1/72 inch

• Cost• Minimize

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1st Generation Project – Class of 2015

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Prioritizing Engineering Characteristics

Customer Requirements Cu

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Engineering Charateristics

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Increased Stability 5 9 3 6 3 9 6 6

Lower Weight 5 3 9 6 3 6 9

Good Images 5 6 9 9 3

Better Horn Mounting 5 9 9 9

Cost 4 3 6 3 3 3 3

Hardware Box 2 3 6 3

Portability 2 6 9 6 9

Score 18 30 24 18 24 27 18 15 21

Relative Weight 78 108 117 90 117 105 72 72 69

Rank 6 3 1 5 1 4 7 7 9

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Most Important EC’s:1. Mounting Mechanism1. Locking Mechanism3. Material Used4. Base Size5. Axis Adjustability6. Structural Thickness7. Height Above Ground7. Number of Crossbars9. Weight

Key:

#1 Important EC

#2 Important EC

#3 Important EC

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Structure: Version 1• 80/20 Design

• Lightweight

• Cheap

• Modular

• Light machining required

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Structure: Version 3

• Increased cross section width from 1.00” to 1.50”

• Added:• Bottom frame• Outer Braces• Brackets

• Possible leveling castors

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69.50 in

66.00 in

20.00 in

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Structure: Version 4

• Increased stability• Extended horizontal bar on

bottom

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Structure: Version 5

• Reduced weight• Change from 1.50” cross

section width bar to 1.00”• Fixed possible radar interference

• Removed horizontal bar, kept protruding struts on bottom

• Increased stability• Added braces at some joints

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Horn Holder:Version 1

• Compatible with 80/20• Independent locking

and adjustability• Compact

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Horn Holder:Version 2• Removed box shell• Refined rotation

locking• Added 80/20

connection

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Horn Holder:Version 3• Clearance

• Moved horn forward in assembly

• Standardization• Small changes in

dimensions

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4.64 in

2.22 in

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Procurement StatusComponent Vendor Product Team

Member(s)Price Purchase Order

Structure 8020 Inc 8020 Hardware Kegan $920 Submitted

Horn Holders OnlineMetal Aluminum Sheet Kaylen $500 Under review

Fastening Hardware

Localhardware store

Bolts, washers, nuts

Desmond

TBD TBD

Assembly Tools Wrenches TBD TBD

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Structure, $920

Horn Holders, $500

Fastening Hardware (Projected), $100

Tools (Projected), $50

Remaining, $3,430

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Budget

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Schedule

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Summary• Review of Project Scope

• Review Previous Progress

• Design Updates

• Procurement

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Future Plans• Submit remaining purchase orders

• Create operational instructions

• Fabrication

• Testing & modification

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Acknowledgements • Sponsor: Northrop Grumman•Mike Blue

•Pete Stenger

• Senior design instructors:• Dr. Nikhil Gupta

• Dr. Chiang Shih

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References1. NASA AirSAR, https://upload.wikimedia.org/wikipedia/commons/a/a6/AirSAR-instrument-

on-aircraft.jpg

2. Radar Tutorial, http://www.radartutorial.eu/20.airborne/pic/sar_principle.print.png

3. Cammuse, Matthew. “SAR Final Presentation.” http://eng.fsu.edu/me/senior_design/2015/team27/Webpage/presentations/Team%20E%2311_Milestone%20%237%20Presentation_%20Final%20Report.pptx. Web 10/18/2015.

4. E11 Milestone – Final Report, http://eng.fsu.edu/me/senior_design/2015/team27/

5. http://www.northropgrumman.com/Photos/pgM_BA-10002_067.jpg

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Questions?

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6in

3in

Structure Version 3Horn Holder Version 2Full Assembly

1/19/2016

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Full Schedule (including deliverables)

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