Ben Houston Camden Mendiola Dan “Klitz” Johnson Dan Rice Monty Prekeris To provide a flexible low power wireless aerial/terrestrial network that allows the user to survey,
Download ReportTranscript Ben Houston Camden Mendiola Dan “Klitz” Johnson Dan Rice Monty Prekeris To provide a flexible low power wireless aerial/terrestrial network that allows the user to survey,
Ben Houston Camden Mendiola Dan “Klitz” Johnson Dan Rice Monty Prekeris
To provide a flexible low power wireless aerial/terrestrial network that allows the user to survey, sense, and respond. Useful for military, police, search and rescue, and/or back country navigation Localized and self managed.
Camden
To design and implement an autonomous quad-copter platform that can remotely sense and relay data to a base station To utilize the IEEE 802.15.4 protocol to create a low power mesh network Camden
Camden
Motors XBee
Quad-copter ATMega 2560
Environmental Sensors Flight Sensors & GPS
Command Station
PC
Command Station
XBee Motors XBee
Third Comm Module
Environmental Sensors Flight Sensors & GPS Camden
SECONDARY GOAL
Manual Flight Command Locate unoccupied air space Perform Autonomous Flight Pattern Manual Return Flight
ELEVATED GOAL Assert UAV Mode and Input GPS Point Autonomous Navigation to GPS Point Perform Autonomous Flight Pattern Autonomous Return Navigation
Camden
Command Station WINDOWS OS PC USB • XBee PRO ZB • 2.4GHz RF • 3.2 km range • 250 Kbps data throughput • XBee Explorer USB IEEE 802.15.4
Zigbee Protocol Dan J.
Motors
• E-Flight Brushless • 1020Kv • 22A max continuous • 2lb nominal payload/motor Motors ESC ZigBee XBee (Serial)
30A ESC’s:
• Allows 35,000 rpm • 40A for 10s Burst • PWM Copter ATMEGA 2560 Flight Sensors
Flight Sensors:
• Barometer – BMP085 • Magnetometer – HMC5843 • Accelerometer – ADXL345 • Gyro – ITG3200 • Ultrasonic range finder – Daventech SFR10 • GPS – USGlobalSat EM-408 • I2C Env. Sensors
Environmental Sensors (tentative)
: • Temperature • Gas • CMOS Camera -
TCM8230MD
Dan J.
Terrestrial Unit Temperature Chemical Sensing Person ○ Heart Rate Second Quad Copter Mirror functionality of former Quad-Copters Dan J.
•
Battery – 11.1 V, 8000mAh High Discharge Li-Po Battery
•
Power Rails – 5V rail for the ATMega 2560, 3.3V for Sensors and XBee
•
MC33269 Voltage Regulator – takes 12V to 5V
•
Logic Level converter – converts 5V to 3.3V for input to XBee and 3.3V to 5V for signals output from XBee
•
Battery Monitor – checks the status of the battery voltage and signals a warning if it is too low. If the battery supply voltage drops even further, the Quadcopter will begin to land.
•
ESCs (Electronic Speed Controller) – Convert PWM signals from the ATMega2560 into signals for the brushless motors.
Dan J.
Flight Sensors(Primary):
• Barometer – Used to measure atmospheric pressure. Allows the flight control to determine height of the Quadcopter and attempt to increase power to motors in order to maintain altitude.
• Magnetometer – Measures the strength of the Earth’s magnet field to get the heading of the Quadcopter • Accelerometer – Measures acceleration of the Quadcopter along the x, y, z axes. • Gyro – Measures radial velocity in terms of roll, pitch, and yaw.
Flight Sensors(Secondary):
• Ultrasonic range finder – Determines distance objects are away from the sensor. Can be used to avoid objects that come within range of the Quadcopter. Can also be used to aid in landing.
• GPS – Gets longitude and latitude coordinates from a satellite which allows the Quadcopter to determine a flight path to its desired location Dan J.
•
Temperature Sensor
– Analog output. (Primary) •
Gas Sensors
– CO, Methane, Hydrogen gas. Analog Output. (Elevated) •
CMOS Camera
– Communicates using I 2 C. (Elevated) •
Heart rate monitor
I 2 C. (Elevated) – Uses a Polar transmitter and communicates through Dan R.
Ultrasonic
Multiple Ultrasonic sensors may cause interference with one another ○ Alternate sets of opposing sensors to fire at different times.
Wide beam width may cause unexpected detection ○ Size down the beam width and use more sensors Motor interference ○ Relocate sensors
Barometer
Propeller interfering with air pressure ○ Encapsulate barometer or shield it from motors
CMOS Camera
Exceed XBee bandwidth ○ Use high compression ○ Stream at lower frames per second ○ Store images locally Dan R.
Ben
Ad hoc On-demand Distance Vector (AODV) Mesh Routing
Allows data packets to traverse multiple nodes (hops) from source to destination Does not necessarily have to be routed through the coordinator AODV Routing Algorithm dictates ever changing and locally stored look up table of nearest one hop neighbors Ben
Digi International has designed the Xbees in a way that allows a PAN to include up to 40 drop-in radio devices in an Ad Hoc configuration.
Ease of use when building a large self healing network.
Ben
ZB Pro RF data throughput: 250 kbps Line of site range: 3.2 km Serial Flow Control via RTS and CTS pins Encryption (adds latency) Sleep Mode(s) Ability to self manage digital and analog sensors Application Program Interface Ben
The API specifies how commands, command responses and module status messages are sent and received from the module using a UART Data Frame.
Follows IEEE 802.15.4 standard Useful for software design 84 byte payload Multiple command features Ben
Software drivers contain algorithms that can build or parse API packets Payloads can contain the following data: Radio Addresses 12 bits of analog sensor data converted to digital at the XBee hardware level Command Status bytes AT commands Embedded System Experience Ben
Risks
Signal Interference Range Power Consumption Bandwidth
Contingency
XBee PRO® ZB Wall Routers ○ Extends signal strength and range of an XBee ZB mesh network ○ Creates additional network pathways for more reliable mesh networking Adjust Sleep Mode settings via XBee firmware Limit amount of simultaneous data output Ben
ATmega2560
Operating Voltage: 5V JTAG Interface Digital I/O Pins: 54 (of which 14 provide PWM output) ADC Pins: 16 UART Ports: 4 SPI Interface I2C Interface 2 External Interrupt Pins DC Current per I/O Pin 40 mA DC Current for 3.3V Pin 50 mA Flash Memory: 256 KB of which 8 KB used by bootloader SRAM: 8 KB EEPROM: 4 KB Clock Speed: 16 MHz Monty
Eclipse C/C++ Dev environment for Arduino Mega
Allows for parallel development of flight programs and control during PCB development
ATMEL Professional Dev Suite intended for low level debugging though JTAG
Need access to JTAG pin outs which the Arduino Mega does not give access to Emulator AVR JTAG ICE device will be used Monty
• • 200Hz Read Gyro Read Accelerometer • 100Hz Flight Controls (Stabilization routines) • 50Hz Process Telemetry • 25Hz Read Barometer • • 10Hz Read Battery Process Compass Monty
ATmega PID MOTORS SENSOR RESPONSE
Monty
Task Scheduling – Addition of sensors consumes clock cycles Scheduling sensors in order of priority Circumvent processer and straight to XBee Co-Processor Hard Real Time System – Sam Monty
•
Prototype Frame
: Made from Balsa, Poplar and Oak. •
Aluminum Frame
: Aeroquad frame that is more robust.
•
Future Frames:
A Carbon Fiber or Fiberglass frame could be used, as these are lightweight at the risk of durability Dan R.
Indoor net and pulley apparatus Emergency Shutoff via firmware watchdog timer Manual Emergency shutoff via a serial command Dan R.
Phase 1:
PCB Design Flight Command
Phase 2:
PCB Revision and Design Environmental Sensor *Hardware design *Software design XBee Mesh Network
Phase 3:
Basic Auto Patterns GPS Integration Ben Camden Daniel Klitz Monty Dan R.
Dan R.
• Frame • Plan to buy Aluminum frame in the future. If it is not available, we may have to make it ourselves.
• Schedule uncertainty • Current timeline does not incorporate weekends.
• Availability of components • Utilize multiple distributers • Code Sharing • Tortoise SVN with revision control • Broken Parts • Backup Parts on hand (Propellers) Dan R.
Component
E-Flite 480 Brushless Motors Hobbywing Pentium 30A ESCs Accelerometer ADXL-345 Magnetometer HMC-5843 Barometer BMP-085 Gyro ITG-3200 XBee ZB Pro 2.4GHz
Arduino Mega2560 Temp Dev. Boards Safe Testing Apparatus 8000 mAH LiPo Battery Revision 1 Frame Materials Revision 2 Aluminum Frame PCB Orders ATMega 2560 QFP Processors US GlobalSat EM-408 GPS Module Other Sensors (Gas, Heartrate, Camera, etc)
#
4 4 1 1 1 1 3 2 1 1 1 1 3 2 1 1
Price
$54 each $23 each $15 $15 $20 $50 $40 each $50 each $75 $55 $30 $225 $65 each $20 each Free, Thanks Nate Bernstein $20 - $100 each Dan R.
Component
Other SMT Board Components Total (Not including tentative high level sensors)
#
3
Price
$50 each ~ $1400 Funding: -UROP -EEF (possible) -Sponsorship through Elintrix Dan R.