Bilag 1: Helikopterens fysiske egenskaber - SmartData

Projekt-navn
Organisation/sted
AVATAR
University of
Southern
California
RAPTOR
University of
Southern
California
Helikopter /
platform
Bergen Industrial
Helicopter (Benzin)
Længde: 1,5 m
Rotor ø: 1,6 m
Vægt 8,2 Kg
Nyttelast ~9,0 Kg
Lite Machine LMH-
110 (Batterier)
Længde 0,67 m
Rotor ø: 0,60 m
Vægt: 0,8 kg (eksl
batt.)
Nyttelast ~1,0 kg
Sensorer Kilde
DGPS (Novatel RT-20).
IMU (Boeing CMIGTS-II INS).
Kamera (Sony Colour CCD ukendt model).
Ultralyds sonar (ukendt fabrikat).
IMU, hjemmebygget (ADXL-202 Analog
Devices, CG-16D NEC Tokin).
Kamera (Spectronix’s Robo-CAM2 CMOS
kamera m. integreret frame-grabber).
Ultralyds sonar (Polaroid 6500 sonar range
finder).
Laser-pointer (ukendt fabrikat).
Saripalli, Srikanth, David J. Naffin og Guarav S.
Sukhatme.
Autonomous Flying Vehicle Research at the
University of Southern California. Proceedings of
First International Workshop on Multi-Robot
Systems, Washington DC 2002.
http://wwwrobotics.usc.edu/~avatar/hardware/hardframe.html
http://www.bergenrc.com/IndustrialTwin.asp
Saripalli, Srikanth, David J. Naffin og Guarav S.
Sukhatme.
Autonomous Flying Vehicle Research at the
University of Southern California. Proceedings of
First International Workshop on Multi-Robot
Systems, Washington DC 2002.
http://wwwrobotics.usc.edu/~dnaffin/Research/research.html