Preliminary Design Review February, 2012 Kody Mallory Adam Prulhiere Bruce Deakyne Luke Tonneman Trevor McDonald The Research and Engineering Center for Unmanned Vehicles (RECUV) is a university, government,
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Transcript Preliminary Design Review February, 2012 Kody Mallory Adam Prulhiere Bruce Deakyne Luke Tonneman Trevor McDonald The Research and Engineering Center for Unmanned Vehicles (RECUV) is a university, government,
Preliminary Design Review
February, 2012
Kody Mallory
Adam Prulhiere
Bruce Deakyne
Luke Tonneman
Trevor McDonald
The Research and Engineering Center for
Unmanned Vehicles (RECUV) is a university,
government, and industry partnership
dedicated to the development and application
of unmanned vehicle systems. RECUV
research encompasses scientific experiments,
commercial applications, mitigation of
natural and man-made disasters, security,
and national defense.
Photo Courtesy of Jack Elston
Photo Courtesy of Jack Elston
The TornadoTrak system will be capable of
maintaining contact with an unmanned aerial
vehicle (UAV) as it flies its route in dangerous
and unstable weather conditions.
Operate at 900 MHz
Omni-directional and electronic beamsteering modes
Autonomous and manual input beamsteering
Interface with existing architecture
Fit on roof of chase van
Primary
◦ Receive desired angle from Mobile Control Station
(MCS) and steer relative to van orientation
Secondary
◦ Combine GPS data from UAV and MCS to determine
desired angle
Tertiary
◦ Use signal quality feedback from transceiver to
finely adjust angle using control law
8 Element Uniform Circular Array
Half Wavelength Radius
Radiating Element: Monopole
900 MHz Monopole Antenna
◦
◦
◦
◦
◦
◦
◦
SMA Connection
Up to 10 W
50 Ω
Cheap
Small
Light-Weight
Durable
Transmit Network
Transceiver
Controller
Receive Network
Antennas
Antenna
Phase Shifter
T/R
Amplifier
Divider
Control Block
Summer
Phase Shifter
T/R
Purpose:
To relay amplitude and phase shifted signal from
source to 8 separate antennas
Parts
◦
◦
◦
◦
T/R Switch
Phase Shifters
Amplifiers
Limiter
T/R
Divider
Antenna
Phase Shifter
Amplifier
Amplifier
T/R
Purpose:
◦ Relay and phase shift data from antenna array to
base station
Utilizes the internal amplifier of the MCS
Parts:
◦
◦
◦
◦
Isolators (if required)
T/R Switch
Phase Shifters
Summer
T/R
Summer
Antenna
Phase Shifter
T/R
JSPHS-100 Variable Phase Shifter
◦ 0-15V Voltage controlled
◦ 700-1000 MHz
◦ 180 degrees, 50 ohm
AD5582 Quad DAC
◦ 12 bit 0-15V output voltage
◦ Read/Write Mode
The microcontroller will interface with the
MCS and UAV for gathering and processing
the location and orientation information
◦
◦
◦
◦
◦
GPS from UAV
Commands from MCS
Control the phase shifters to steer beam.
GPS and Magnetometer from MCS
Communicate with Transceiver
uC Accuracy
◦ 32 Bit FP unit
Timing requirement- control a 1 degree
margin within 0.87 seconds
◦ Omni mode is enabled at ~1km
◦ UAV Speed=20m/s
GPIO=~30 Pins
SCI communication
MCS
Phased
Array
RF Signal
Digital Signal
Analog Signal
Command (USB/SCI)
GPS/Magnetometer Data
DAC Select [1:0]
DAC Mode [3:0]
uC
DAC φ Value[11:0]
DAC Read φ [11:0]
Signal Strength
Command
RS232
AMP
(x8)
Quad
DAC
(x4)
Voltage
Phase
Shifter
(x8)
TX Signal
Phase
Shifter
(x8)
Transceiver
TX Data
(From MCS)
RX
Signal
TMS320F28035
◦
◦
◦
◦
32 bit 60MHz with floating point arithmetic unit
SCI/SPI/I2C Interfaces
1.8/3.3v supply
45 GPIO pins
USB Interface
◦ FT232RL
System will be powered by the MCS
This is 120 V AC 60 Hz
Converters need to rectify AC input voltage to
DC output voltage
◦ Need 1.8 V, 3.3 V to power ICs
◦ Also need 15 V for reference for DACs
◦ Will also need to monitor current, as too much
might damage some components
Will have two stages: Commercial rectifier,
and then linear regulators
◦ Linear regulators will provide the needed voltages
Outputs will need to be monitored to control
current output
◦ Outputs will additionally be fused to prevent
damaging current spikes
Try to have isolation transformers between
different power stages
◦ Done to reduce interference from ground loops
Special attention to the layout of the PCBs
with RF traces
◦ Due to high frequency, could run into EMI and
coupling into the power and ground plane.
Converters will have a separate PCB, and
power will be routed to each individual
system
◦ Promotes modularity
Design for highest efficiency possible
◦ MCS does not have unlimited power
15 V
reference
120 V AC
from MCS
Converter
system, 15
V reference
and 3.3 V,
1.8 V for ICs
3.3 V, 1.8 V
supply
DACs
Microcontroller,
DACs,
Amplifiers, USB
Interface
120 V
AC
Commercial
rectifier
providing 15
V DC
Linear
Regulators
Load
Capacitors– Mouser Electronics
◦ For bypass, decoupling and various other purposes
POWER SUPPLY EXT - CENB1010A1503B01
◦ Supplies 12W 15V @ 0.8A
Linear Technology LTC1844 Linear Regulator
◦ Adjustable output voltages
Coilcraft DA2303-AL Isolation Transformers
◦ To minimize ground loops
Van Power
Antenna
Power Systems
Magnetometer
Microcontroller
Serial Data
Amplifiers /
Phase Shifters
Requirements:
◦ Durable
◦ Weatherproof
◦ Lightweight
Antenna Mount
Antenna Ground Plane
Materials:
◦ Plexiglass (Acrylic)
◦ Aluminum
◦ PVC
Shielding
PCB
Processor can’t keep up with UAV
◦ Reduce Tracking resolution and resort to Omni
mode further out
USB Interface is non communicative
◦ Revert to module made by Sparkfun and connect
Feedback is not accurate enough
◦ Resort to assuming correct response
DAC accuracy
RF network error
◦ Calibrate in chamber and modify software
Reflection
◦ Matching network
Component noise
◦ Calibration
Signal Delay
◦ Transceiver settings
Might not be able to incorporate isolation
transformers
◦ Redesign PCB to minimize ground loop size
Interference could be produced from the
lines, traces on the PCBs
◦ Shielding
Modular System
◦ Easy repair in the field
Shielding between PCB and RF
Beam Steering Failure
◦ Switched beam high gain antenna
Very little team CAD or fabrication experience
◦ Utilize colleagues in MechE
Adequate shielding
◦ RF power meter
Durability & Weight
◦ Safety margins
Schedule “Troubleshoot week”
Reallocate resources as necessary
Phase project
◦ Working individual components
RF and Antenna
Quantity
Price
Total Cost
Variable Phase
Shifter
36
$26.95
$970.20
8 Way Power
Splitter/Combiner
2
$138.95
$277.90
Fixed Gain
Amplifier
8
$84.95
$679.60
T/R Switch
9
$56.95
$512.55
Monopole
Antenna
8
$9.95
$79.60
RF Cables
52
$8.45
$439.40
RF Total
$2,959.25
Embedded &
Analog
Quantity
Price
Total Cost
Microprocessor
1
$83.07
$83.07
DAC
4
$19.58
$78.32
Connector
1
$1.29
$1.29
USB-Serial
1
$6.99
$6.99
E&A Total
$169.67
Power
Quantity
Price
Total Cost
PCBs
15
$30.00
$450.00
Filter Capacitors
20
$1.55
$1.55
Linear Regulators
3
$1.77
$5.31
Isolation
Transformer
3
Sampled
$0
Power Supply
1
$14.38
$14.38
Power Total
$471.24
Hardware
Quantity
Price
Total Cost
Plexiglas
1
$110.00
$110.00
Mounting
1
$25.00
$25.00
Hardware
1
$50.00
$50.00
Aluminium Sheet
1
$40.00
$40.00
Poster
1
$50.00
$50.00
Misc. Total
$275.00
Total Projected Cost
$3,875.16
Organization
Amount
Undergraduate Research
Opportunity
$1,000
Engineering Excellence
Fund
$1,000
Research and Engineering
Center for Unmanned
Vehicles
$5,000
Total
$7,000
Task
Kody
Control Algorithm
P
S
Comm SW
P
S
Adam
Power Board
Luke
Trevor
P
S
Array Design
P
S
Beam Forming
Network
S
P
Controller Board
P
RF Boards
P
Mount/Structure
Sensor Interface
S
S
S
S
S
S
S
S
S
P=Primary
Bruce
P
P
S=Secondary
RECUV, Professor B. Argrow, Jack Elston and
Maciej Stachura
Joe Carey, Fidelity Comtech
Brandon Gilles, First RF
Professors E. Kuester, D. Filipovic
Tom Brown, Sam Siewert
Carissa Pocock, Robert Pomeroy, Jeries
Shihadeh