LinkMAV, A protoype rotary wing micro aerial vehicle

IFAC Proceedings Volumes (IFAC-PapersOnline)

Volumn 17, Issue PART 1, 2007, Pages 473-478

  Duranti, S ^a   Conte, G ^a   Lundstrom D ^a   Rudol, P ^a   Wzorek, M ^a   Doherty, P ^a  

^a LINKÖPING UNIVERSITY   (Sweden)

Author keywords

Control and navigation; Design; Helicopter; UAV dynamics

Indexed keywords

AIR NAVIGATION; ANTENNAS; AUTOMATION; DESIGN; FLIGHT CONTROL SYSTEMS; FREE FLIGHT; HELICOPTERS; WINGS;

AUTONOMOUS NAVIGATION; COLLISION-FREE PATH-PLANNING; FLIGHT MISSION; FLYING PLATFORMS; HIGH-LEVEL SYSTEMS; MICRO AERIAL VEHICLE; MULTI-MODAL INTERFACES; ONBOARD AVIONICS;

MICRO AIR VEHICLE (MAV);

EID: 79960999942     PISSN: 14746670     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.3182/20070625-5-fr-2916.00081     Document Type: Conference Paper

References (3)

1. Colin P. Coleman. A survey of theoretical and experimental coaxial rotor aerodynamic research. March 1997.
2. MAV05. First American-European MAV Competition. www.as.go.dlr.de/MAV05/.
3. M. Tischler, B. Mettler, and T. Kanade. System identification modeling of a model-scale helicopter. CMU-RI-TR-00-03, 2000.