Transition flight of quad tilt wing VTOL UAV

28th Congress of the International Council of the Aeronautical Sciences 2012, ICAS 2012

Volumn 4, Issue , 2012, Pages 3242-3251

  Muraoka, Koji ^a   Okada, Noriaki ^a   Kubo, Daisuke ^a   Daisuk, Masayuki ^a  

^a JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

Author keywords

Flight test; Simulation; Tilt wing; UAV; VTOL

Indexed keywords

AUGMENTATION SYSTEMS; FLIGHT TEST; SIMULATION; SIX-DEGREE-OF-FREEDOM; TILT-WINGS; TRANSITION FLIGHT; VERTICAL TAKE-OFF; VTOL;

COMPUTER SIMULATION; FLIGHT CONTROL SYSTEMS; UNMANNED AERIAL VEHICLES (UAV);

FLIGHT SIMULATORS;

EID: 84881486043     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (5)

1. Anderson S. Historical Overview of V/STOL Aircraft Technology. NASA-TM-81280, 1981.
2. Muraoka K, Okada N, and Kubo D. Quad Tilt Wing VTOL UAV: Aerodynamic Characteristics and Prototype Flight Test, AIAA Infotech@Aerospace Conference, AIAA-2009-1834, 2009.
3. Kubo D, Moriyama N, Muraoka K and Tsukamoto T, Development of a Flight Control System for Small Experimental UAVs and Flight Tests, Proc 49th JSASS Aircraft Symposium, 2A3, 2011 (in Japanese).
4. Sato M, Muraoka K, Okada N and Kubo D, Attitude Controller Design for Quad Tilt Wing-type VTOL UAV, Proc SICE 28th Symposium on Guidance and Control, 2011 (in Japanese).
5. Sato M, Muraoka K, Okada N and Kubo D, Flight Controller Design for Quad Tilt Wing-type VTOL UAV, Proc JSASS 43rd Annual Meeting, D17, 2012 (in Japanese).