Project files are stored in SVN repository (registration required). Remote access is possible by SVN client TortoiseSVN for example. Repository is public for reading, but requires account for write access. If you are interesten in contribution drop email to kaklik@mlab.cz please.

• Konstrukce

Required features:

• 10Hz update rate
• Airspeed (min 16m/s, avg 22,3 m/s, max 30m/s) 600Pa max
• Barometer (Air density, altitude)
• Humidity sensor (Fail safe, Air density)
• Temperature sensor (Fail safe, Air density)
• Camera?
• Battery Voltages, Currents (Battery gas gauge)
• Engine power sensing, max engine current 30A.
• GPS
• IMU (Akcelerometers -3G to 5G)
• Magnetometer

Non fly prototype is build from MLAB prototyping modules. Photo

PPM Decoder/DeMultiplexer is build from ATmegaTQ3201A populated by ATmega328 and 16MHz crystal.

Main UAV control board is based on STM32F10xRxT01A ARM microcontroller module. datasheet

• Airspeed - Differential pressure.

• u-blox LEA-6S module.
• VTGPSIA-3 GPS patch antenna

Some resistive current measurement sensor with analog output and voltage divider to 3,3V range.

Classical barometric BMP085 pressure and altimeter sensor. And GPS data.

Absolute terrain altimeter is necessary for correct landing procedure. It can be resolved by several methods laser, ranging, radar ranging, camera terrain angle speed measurement, camera laser trigonometry, and sonar ranging.

We would use the simplest sonar ranging method at beginning.

• IMU-3000

• ADXL345

• MAG3110
• HMC5883L

Telemetry will be realized by UART ascii output in NMEA like format. Telemetry modules.

Another considered variant is use of some more powerfull telemetry modules Radiometrix modules or Laird Technologies AC4868

• SDcard01B - SD card module.

We will use the JETImodel RC receiver JETI Duplex RSAT2 Some interesting capability of JETI Duplex technology is duplex comunication between receiver and transmitter. So telemetry download via JETI Duplex RC receiver could be possible. Old JETI Duplex V1 protocol specification

Ideas

Bachelor's thesis about foundation for our control algorithms. Marián Šuch 2012

The autopilot software control algorithm will be tested by hardware in loop configuration. Where autopilot hardware will be physical but model of airplane and avionic will be numerically simulated.

Provedeni DGPS: Pozemni stanice bude vysilat vlastni telemetrii, ktera bude obsahovat DGPS korekce. Ty se v UAV pouziji pro vypocet polohy, ktera se opet telemetrii odesle do pozemni stanice. Navigace tak bude v podstate rozdilova proti pozemni stanici. To umozni snazsi definovani bodu trasy a nasledne i pripadne zjednodussi budouci moznost pristavani pobliz pozemni stanice.

• USB232R01B USB to serial converter.

• ATprogISPUSB02A AVR micro-controller programmer.

• Eigen
  
  • some algorithms will use quaternions to prevent gimbal lock

• ChibiOS
  
• FreeRTOS

• Ivan Jerabek
• Jakub Kákona - kaklik@mlab.cz
• Marian Such
• .
• .
• .

Other similar known projects for reference:

• http://paparazzi.enac.fr/wiki/Main_Page
• CVUT RAMA http://rtime.felk.cvut.cz/helicopter/
• http://pixhawk.ethz.ch/wiki/
• http://code.google.com/p/ardupilot-mega/
• http://www.openpilot.org/
• http://gluonpilot.com/wiki/Main_Page
• http://code.google.com/p/gentlenav/
• http://slugsuav.soe.ucsc.edu/index.html
• http://www.sensesoar.ethz.ch/doku.php?id=solar_airplane_design#autopilot

Model parameters and radio transmissions limits (cz only)
Postupy pro vydání povolení k létání letadla bez pilota na palubě (UCL)