Project ASD (Aerial Surveillance Drone)

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Project ASD
(Aerial Surveillance Drone)
TEAM SYNTECH
KEN, ANDY, DAN, TRAVIS, RYAN
1/25/2011
Overview
Team Syntech’s objective is to construct an
autonomous quad copter that performs aerial
maneuvers and reconnaissance functions.
Team Syntech
Redington, Ryan Le, Cartwright, McCormick, Hua
1/25/2011
Objectives (Low)
 Micro Controller
commanding motors
 Autonomous stable
hovering
 Safety measures (Basic
Wireless Features)


Emergency remote kill
switch (copter goes dead)
Remote hover button: copter
returns to stable hover state
 Turning
 Planar movement
 LED’s
Team Syntech
Redington, Ryan Le, Cartwright, McCormick, Hua
http://www.isys.unistuttgart.de/forschung/mechatronik/robo/quadk
opter/index.en.html
1/25/2011
Objectives (Med)
 Collision durability
 Altitude adjustment
 Navigation using a system of beacons
 Can carry payload (specifically a digital camera)
 Recording pictures and/or video
 Wireless communication to a base station
Team Syntech
Redington, Ryan Le, Cartwright, McCormick, Hua
1/25/2011
Objectives (High)
 High altitude capabilities
 Spotlight LED
 Communication of video/picture to base station
 Pan/Tilt of the camera
 Obstacle avoidance
 Inductive charging at a base station
Team Syntech
Redington, Ryan Le, Cartwright, McCormick, Hua
1/25/2011
Software
Environment
Motor Control
Control Algorithms
Body
Controller
Remote kill switch
Frame
Microcontroller
Beacons
Motors
Altimeter
Sensor I/O
Power Mat
Main Battery
Inclinometer
Kill switch
Data Receiver
Camera
Z-Accelerometer
Wireless I/O
Remote Control
LEDs
Power Monitor
Programmer
Main Power
Aux Power
LED Control
Aux Battery
Data Manager
Wireless
Motor Driver
Navigation
Serial
Boot loader
LEDs
Team Syntech
Redington, Le, Cartwright, McCormick, Ken Hua
1/25/2011
Software
Microcontroller
Camera
LEDs
Aux Pwr
Motor Drive
Main Pwr
Serial
Aux Batt
Motors
Main Batt
Power Mat
Props
Team Syntech
Sensors
Beacons
Redington, Le, Cartwright, McCormick, Ken Hua
Wireless
Bootloader
LEDs
Programmer
Remote
Data Receiver
1/25/2011
Implementation
Micro controller
-Atmel B series
-AT32UC3B0256.
-256KB FLASH 64-TQFP.
64 Pin Atmel Microcontroller
Sensor
-VTI Inclinometer DUAL 1G DIL12 SMD
-SCA100T-D02
-X/Y tilt control data.
VTI Inclinometer
Team Syntech
Daniel Redington, Le, Cartwright, McCormick, Hua
1/25/2011
Implementation
Dual Power Systems
•Main Power
•Lithium Polymer
•Triple Cell
•11.1V
•2250mAh
•Supply for Motors
•Auxiliary Power
•Small- Single Cell Battery
•Supply for electronics and
Microcontroller
Team Syntech
DanielRedington, Le, Cartwright, McCormick, Hua
1/25/2011
Implementation
Flight Characteristics
•5” Propeller
•Motor
•0V-11V
•4000 (RPM/V)
•Max RPM (no load): 42k RPM
•Weight: 40-70g
Theoretical Load
•Total Weight 497g + x
•4x Motors = 160-280g
•Li Poly = 180g
•2x Carbon Fiber Plate = 13g
•4x 5” Carbon Fiber Tube = 24g
•Other Materials = x (g)
•Static Thrust per motor
•15k RPM = 180g lift
•20k RPM = 330g lift
•25k RPM = 510g lift
•30k RPM = 740g lift
•Estimated copter lift
•4x Motors @ 16k RPM
•800g Lift
Team Syntech
Redington, Le, Travis Cartwright, McCormick, Hua
1/25/2011
Risks and Contingencies
 Broken Parts during testing
 Ordering multiples of parts
that are likely to be broken
 Insufficient thrust to lift
payload


Bigger propeller
Adjust battery size
 Overall Project Structural
Failure

member(s)

Purchase a commercial quad
copter body kit
 Over budget
 Remove the camera from plan
 Materials for construction
Team Syntech
 Not enough time
 Reduce features/capabilities
from low category
 Going out of control
 Netting and a tether
 Kill switch and hover switch
 Unavailability of team

Shift work to other members
Reduce features/capabilities
 Controller does not work
 Buy off the shelf components
(Arduino)
Redington, Le, Travis Cartwright, McCormick, Hua
1/25/2011
Division of Labor and Responsibilities
 Travis Cartwright
 Embedded Design
 Software Developer
 Ken Hua
 Software Dev Lead
 Frame Construction
 Sub versioning Admin
 Documentation
 Andy McCormick
 Team Lead/Administrator
 Power Systems
 Budgeting/Scheduling
 Documentation Lead
 Daniel Redington
 Embedded Design Lead
 Software Developer
 Ryan Le
 Software Dev Lead
 Documentaion
 Frame Construction
Team Syntech
Redington, Le, Cartwright, Andy McCormick, Hua
1/25/2011
Budget
Part
Description
Micro Controller
And components
Cost ($)
The B Series AVR 256KB FLASH 64-TQFP
50.00
VTI Inclinometer DUAL 1G DIL12 SMD
150.00
Advanced Integrated Circuitry (2 revisions)
100.00
Motors and Drivers
4 Brushless EDF Outrunner with 4000 RPM/V
150.00
Camera and Mount
Mountable camera for surveillance video recording/transmission
100.00
2 Thunder Power 2250 mAh LiPoly
115.00
0.015 in. Twill-Weave Carbon Fiber Sheet 11 in. x 8 in.
60.00
GWS EP Propeller 127x76mm, screws, epoxy, spacers, motor casing,
mounting hardware
50.00
Printing
PDR, CDR, Final draft of Users manual
130.00
Total
All parts and Components needed
$905.00
Sensors
PCB
Batteries
Carbon Parts
Props & Hardware
Team Syntech
Redington, Le, Cartwright, Andy McCormick, Hua
1/25/2011
Schedule
By Preliminary Design Review –
• Get the initial version of the
users manual written
• Set up SVN for code
repository
• Begin core circuit design
• Fill out the UROP funding
form
• Order test parts
• Order batteries
Team Syntech
By Critical Design Review –
• Finish Core and Peripheral
circuit design
• Draft and finalize the board
layout
• First revision of prototype
controller
• First round of software
implementation
• Finalize body design
Redington, Le, Cartwright, Andy McCormick, Hua
1/25/2011
Schedule
Milestone 1 –
• Motor and power systems
functional
• Chassis built
• Hover functionality designed
and functional
Team Syntech
Milestone 2 –
• Functional turning
• Ascend/descend code
compiled
• Establish wireless
communication
Redington, Le, Cartwright, Andy McCormick, Hua
1/25/2011
Functional Gantt Chart
Team Syntech
Redington, Le, Cartwright, Andy McCormick, Hua
1/25/2011
Questions?
Team Syntech
Redington, Le, Cartwright, McCormick, Hua
1/25/2011
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