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Radar Interface Design Project Final Presentation Sponsor: Scott Faulkner, Lockheed Martin Group #1 Catherine Donoso Diego Rocha Keith Weston

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Page 1: Radar Interface Design Project Final Presentation Sponsor: Scott Faulkner, Lockheed Martin Group #1 Catherine Donoso Diego Rocha Keith Weston

Radar Interface Design Project

Final Presentation

Sponsor: Scott Faulkner, Lockheed Martin

Group #1Catherine DonosoDiego RochaKeith Weston

Page 2: Radar Interface Design Project Final Presentation Sponsor: Scott Faulkner, Lockheed Martin Group #1 Catherine Donoso Diego Rocha Keith Weston

Overview

• Power Supply (PS) for transceiver in Joint Air to Ground Missile (JAGM) seeker

• PS system must generate specific voltages

• PS system must use power sequencing

• PS must include control unit

Page 3: Radar Interface Design Project Final Presentation Sponsor: Scott Faulkner, Lockheed Martin Group #1 Catherine Donoso Diego Rocha Keith Weston

Goals• Lowest heat dissipation possible when selecting parts

• limited airflow

• No heat sink available directly on board, only for system

• Less surface area on the board

• Update design to utilize new technology

• Non-Rohs Compliant

• Military Grade Temperatures , -55° to +125° Celcius

Page 4: Radar Interface Design Project Final Presentation Sponsor: Scott Faulkner, Lockheed Martin Group #1 Catherine Donoso Diego Rocha Keith Weston

Specifications

• 32V and 3.3V provided

• 3W of heat dissipation

• 6.3 sq. in board, any shape

• High power architecture

– +6V

– load- less than 50% duty cycle and applied no longer than 100us

– pulse repetition rate from 1 to 100 kHz

• Low power architecture

– -4V, +6V, +9V

– load-continuous

• Control unit

– Power sequencing--4V,+6,+9,+6(high)

– Current sensing

– Temperature sensing

Page 5: Radar Interface Design Project Final Presentation Sponsor: Scott Faulkner, Lockheed Martin Group #1 Catherine Donoso Diego Rocha Keith Weston

Power Section

• Specs for the four different voltages.

Signal Output Voltage Output Current Regulation Ripple Voltage

6XMIT 6VDC 11 A 3% 1mV

9XCVR +9VDC 100mA 3% 100uV

6XCVR +6VDC 1000mA 3% 100uV

4XCVR -4VDC 250mA 3% 100uV

Page 6: Radar Interface Design Project Final Presentation Sponsor: Scott Faulkner, Lockheed Martin Group #1 Catherine Donoso Diego Rocha Keith Weston

9XCVRNetwork for Simulation in LTspice

Actual Network Implemented

Page 7: Radar Interface Design Project Final Presentation Sponsor: Scott Faulkner, Lockheed Martin Group #1 Catherine Donoso Diego Rocha Keith Weston

9XCVR Simulation Results

Transient Steady State

Page 8: Radar Interface Design Project Final Presentation Sponsor: Scott Faulkner, Lockheed Martin Group #1 Catherine Donoso Diego Rocha Keith Weston

6XCVRNetwork for Simulation in LTspice

Actual Network Implemented

Page 9: Radar Interface Design Project Final Presentation Sponsor: Scott Faulkner, Lockheed Martin Group #1 Catherine Donoso Diego Rocha Keith Weston

6XCVR Simulation Results

Transient Steady State

Page 10: Radar Interface Design Project Final Presentation Sponsor: Scott Faulkner, Lockheed Martin Group #1 Catherine Donoso Diego Rocha Keith Weston

6XMIT High Power Simulation in LTspice

Page 11: Radar Interface Design Project Final Presentation Sponsor: Scott Faulkner, Lockheed Martin Group #1 Catherine Donoso Diego Rocha Keith Weston

Spreading SpectrumFrequency Spectrum using technique Frequency Spectrum without using

technique

Page 12: Radar Interface Design Project Final Presentation Sponsor: Scott Faulkner, Lockheed Martin Group #1 Catherine Donoso Diego Rocha Keith Weston

6XMITActual Network Implemented

Page 13: Radar Interface Design Project Final Presentation Sponsor: Scott Faulkner, Lockheed Martin Group #1 Catherine Donoso Diego Rocha Keith Weston

6XMIT Simulation ResultsTransient Steady State

Page 14: Radar Interface Design Project Final Presentation Sponsor: Scott Faulkner, Lockheed Martin Group #1 Catherine Donoso Diego Rocha Keith Weston

Timing and Control System• The goals for the timing and control architecture’s will be to:

• monitor and power sequence the subsystems

– -4V, +6V(low), +9V, +6V(High)

– exact opposite for power down• Communicate and interpret commands from the missile i.e. power up/ power

down• Provide feedback as to the subsystems functionality i.e. voltage and currents are

operating within tolerance

Page 15: Radar Interface Design Project Final Presentation Sponsor: Scott Faulkner, Lockheed Martin Group #1 Catherine Donoso Diego Rocha Keith Weston

Timing and Control System (2)

• We looked at different devices to solve our problems including:– Microcontroller, CPLD, and

FPGA– We leaned towards an

FPGA after we found the Actel Fusion FPGA that integrated the volatile memory and A/D convertors into the chip reducing board space considerably.

Page 16: Radar Interface Design Project Final Presentation Sponsor: Scott Faulkner, Lockheed Martin Group #1 Catherine Donoso Diego Rocha Keith Weston

Analog Quads

• Analog quads allow us to directly input analog signals (Voltage, Current and Temperature)

• This is a four channel system used to precondition analog signals before sending the signal to the A/D Convertor. The QUAD has four blocks. We will be using two of them.

• The 1st is aVoltage monitor. It allows an analog voltage signal to be routed to the pre-scalar where it is scaled to an acceptable input voltage and sent to the A/D Convertor

Page 17: Radar Interface Design Project Final Presentation Sponsor: Scott Faulkner, Lockheed Martin Group #1 Catherine Donoso Diego Rocha Keith Weston

Analog Quads (2)

• The 2nd block is the current monitoring block (AC Pin) It uses a external current sense resistor to measure a voltage across the AV AC pin.

• Depending on measured current a resistor size is selected from the chart

Recommended Resistor for Different Current Range Measurement

Current Range Minimum Resistor Value (Ohms)

> 5 mA – 10 mA 10 - 20

> 10 mA – 20 mA 5 - 10

> 20 mA – 50 mA 2.5 - 5

> 50 mA – 100 mA 1 - 2

> 100 mA – 200 mA 0.5 - 1

> 200 mA – 500 mA 0.3 - 0.5

> 500 mA – 1 A 0.1 - 0.2

>1A–2A 0.05 - 0.1

>2A–4A 0.025 – 0.05

>4A–8A 0.0125 – 0.025

> 8 A – 12 A 0.00625 – 0.02

Page 18: Radar Interface Design Project Final Presentation Sponsor: Scott Faulkner, Lockheed Martin Group #1 Catherine Donoso Diego Rocha Keith Weston

Software Development Environment

• ACTEL FUSION STARTER-KIT was used for software development

• Same exact FPGA model and die as used in our project which eliminated pin differences problems

• Onboard circuitry and software highlighted boards strengths.

Page 19: Radar Interface Design Project Final Presentation Sponsor: Scott Faulkner, Lockheed Martin Group #1 Catherine Donoso Diego Rocha Keith Weston

Software Development

• Actel Libero IDE 8.6 Advantages

• Many implemented design ideas and tutorials available for download

• Many IP Cores had graphical interface which made designing modules easier

Page 20: Radar Interface Design Project Final Presentation Sponsor: Scott Faulkner, Lockheed Martin Group #1 Catherine Donoso Diego Rocha Keith Weston

IP Core for Analog Monitoring

Page 21: Radar Interface Design Project Final Presentation Sponsor: Scott Faulkner, Lockheed Martin Group #1 Catherine Donoso Diego Rocha Keith Weston

Analog Voltage Setup

Page 22: Radar Interface Design Project Final Presentation Sponsor: Scott Faulkner, Lockheed Martin Group #1 Catherine Donoso Diego Rocha Keith Weston

Analog Current Setup

Page 23: Radar Interface Design Project Final Presentation Sponsor: Scott Faulkner, Lockheed Martin Group #1 Catherine Donoso Diego Rocha Keith Weston

Current Monitoring

• Evaluation Board Measuring the AFS 600 Core Current

Page 24: Radar Interface Design Project Final Presentation Sponsor: Scott Faulkner, Lockheed Martin Group #1 Catherine Donoso Diego Rocha Keith Weston

Voltage Monitoring

• Evaluation Board Measuring the AFS 600 Core Voltage

Page 25: Radar Interface Design Project Final Presentation Sponsor: Scott Faulkner, Lockheed Martin Group #1 Catherine Donoso Diego Rocha Keith Weston

Temperature Monitoring

• Evaluation Board Measuring Temperature measured by Q8 on the evaluation Board

Page 26: Radar Interface Design Project Final Presentation Sponsor: Scott Faulkner, Lockheed Martin Group #1 Catherine Donoso Diego Rocha Keith Weston

PCB Layout (1)• Only 6.6 sq. in.,

• Parts were installed only on topside

• Number of layers is 6

• Stackup of layers must be balanced

– Bottom layer balances the stackup

– Prevents board from warping

• Signal layers surrounded by plane layers

• Limit size of part

– Used 2.2uF 100V capacitors take less space than 10uF

• Ball grid array (BGA)

– FPGA

• Capacitors near to reduce wire length that introduces noise

POWERBOTTOM

SIGNAL

SIGNAL

GROUND

TOP

Page 27: Radar Interface Design Project Final Presentation Sponsor: Scott Faulkner, Lockheed Martin Group #1 Catherine Donoso Diego Rocha Keith Weston

PCB Layout (2)• 6 sq. in alloted on template• Guides

– Show what is connected– Disappear during routing as

parts are connected– Nets cannot hook up wrong

pins• Each active component should

have its respective passive components near it

• Must have a relative flow between each part to make routing easier and cleaner

• 0.025 in component spacing• 0.005 in edge spacing

Page 28: Radar Interface Design Project Final Presentation Sponsor: Scott Faulkner, Lockheed Martin Group #1 Catherine Donoso Diego Rocha Keith Weston

Orientation of LTM4612•LTM4612 parts are wired in parallel

•Recommended to orient parts same and have identical passive component layout and identical wire lengths to work efficiently

•Parts are oriented 180 degrees. •Surrounding parts fit around better with board space constraints

•RUN pin was set to have identical wire length •Wire can zig-zag if necessary

Page 29: Radar Interface Design Project Final Presentation Sponsor: Scott Faulkner, Lockheed Martin Group #1 Catherine Donoso Diego Rocha Keith Weston

Final PCB Layout•Extra copper laid for heat dissipation below part•More surface area for heat to dissipate•Linear regulator•Dc Dc converter•High current output connector

•3.4x2.6 in. includes test card portion•w/o test card 3.3x2.0 in.•Bottom portion is the test card for low power•High power connector for separate test card•Switches for loads•Max output current•Half output current•No output current•LED •Output voltage indicator•Temperature sensor•JTAG connector•Spare FPGA IO e-points

 

Page 30: Radar Interface Design Project Final Presentation Sponsor: Scott Faulkner, Lockheed Martin Group #1 Catherine Donoso Diego Rocha Keith Weston

Routing (1)• Trace widths defined

– Used calculator• Calculation based on current

and copper thickness• Unless specifically defined, trace widths

0.005 in• Space between traces and parts

determined– 0.005 in

Page 31: Radar Interface Design Project Final Presentation Sponsor: Scott Faulkner, Lockheed Martin Group #1 Catherine Donoso Diego Rocha Keith Weston

Routing (2)• Ball grid array (BGA)

– Dog bones

• Run traces from pad to via

– Pad is 0.024 in. and via is 0.006 in.

• Default vias 0.039 in. pad and 0.012 in. via

• Fan out

– Runs short trace between surface pads to vias

• Useful for BGAs

• Remainder has to be manually routed. Person routing can judge if via needs to be laid or better path for trace

Page 32: Radar Interface Design Project Final Presentation Sponsor: Scott Faulkner, Lockheed Martin Group #1 Catherine Donoso Diego Rocha Keith Weston

Gerber Files Layer 1• The file format sent to the manufacturer for

fabrication are the gerber files• Top layer did not allow for many layers

– Size of board and amount of parts required two layers of signals due to lack of space

• Traces can run to other layers– Thermal relief pads

Page 33: Radar Interface Design Project Final Presentation Sponsor: Scott Faulkner, Lockheed Martin Group #1 Catherine Donoso Diego Rocha Keith Weston

Layer 2 (Ground)

• Analog and digital grounds were isolated on the same plane

• Test portion isolated from remainder

Page 34: Radar Interface Design Project Final Presentation Sponsor: Scott Faulkner, Lockheed Martin Group #1 Catherine Donoso Diego Rocha Keith Weston

Layers 3 & 4 (Signal Layers)• Goal is to have all traces on a layer be

parallel and go one direction– Assures traces can go across

layer without running into another traces

– If trace will cross another, must drop via and go to another layer

• Next signal layer has traces perpendicular to avoid cross talk

• 32 V runs on these layers

Page 35: Radar Interface Design Project Final Presentation Sponsor: Scott Faulkner, Lockheed Martin Group #1 Catherine Donoso Diego Rocha Keith Weston

Layer 5 (3.3V Power Plane)

• Dedicated plane to 3.3V

• Many inputs of 3.3V in circuitry– Multiple pins for

FPGA– Input voltage for

voltage line– Pull up resistors– Biasing on transistor

Page 36: Radar Interface Design Project Final Presentation Sponsor: Scott Faulkner, Lockheed Martin Group #1 Catherine Donoso Diego Rocha Keith Weston

Remaining Gerber Files• Layer 6 (Bottom Layer)

Solder mask Not applied due to lack of

resources

Drill Data 0.0079 in vias

Page 37: Radar Interface Design Project Final Presentation Sponsor: Scott Faulkner, Lockheed Martin Group #1 Catherine Donoso Diego Rocha Keith Weston

Fabrication• In-house fabrication• Available PCB

manufacturers supported max. 6 layers– Wanted the flexibility if

more layers were needed

• Used 0.5 oz. copper• Used chemical etching• Fiberglass used for

dielectric between each layer

• Impedance test not conducted

Page 38: Radar Interface Design Project Final Presentation Sponsor: Scott Faulkner, Lockheed Martin Group #1 Catherine Donoso Diego Rocha Keith Weston

BudgetLinear Technologies LT1963 Linear

Regulator 4 $10.00 $40.00

Linear Technologies LT4612 Switching Power Supply

3 $60.00 $180.00

FPGA Actel Fusion AFS250-QN180I 1 $70.40 $70.40

Actel Fusion Starter Kit 1 $500.00 $500.00

Connectors 2 $30.00 $60.00

Linear Technologies LT8023 Switching Power Supply

3 $60.00 $180.00

Misc (Res,CAPS etc…)

Total $1,044.40

Page 39: Radar Interface Design Project Final Presentation Sponsor: Scott Faulkner, Lockheed Martin Group #1 Catherine Donoso Diego Rocha Keith Weston

Testing Prototype

TI 2808 DSP

• Familiarity with 2808 DSP board facilitates test set up.

• PWM pins have been coded to generate waveforms that can range between 1kHz to 100kHz with a duty cycle that can be varied from 0 to 50%.

• 200kW resistor load bank available for testing.

Page 40: Radar Interface Design Project Final Presentation Sponsor: Scott Faulkner, Lockheed Martin Group #1 Catherine Donoso Diego Rocha Keith Weston

Test set up

Page 41: Radar Interface Design Project Final Presentation Sponsor: Scott Faulkner, Lockheed Martin Group #1 Catherine Donoso Diego Rocha Keith Weston

Proving the Design

• Will not be installed in missile seeker, therefore needs to be proven to work outside of actual system

• Mock loads must be created to effectively test power supply

• High power architecture will have separate test card

• Prototype only purpose, test card will be implemented on same board

• Low power architecture will have onboard test card

• Logic analyzer used to time power sequence