Flight modeling and experimental autonomous hover control of a fixed wing mini-UAV at high angle of attack

Collection of Technical Papers - AIAA Guidance, Navigation, and Control Conference 2007

Volumn 5, Issue , 2007, Pages 4729-4742

  De Blauwe, Hugo ^a,d,e   Bayraktar, Selcuk ^b,f   Feron, Eric ^b,e,f   Lokumcu, Fatih ^c  

^a UNIVERSITY OF LEUVEN   (Belgium)

^b GEORGIA INSTITUTE OF TECHNOLOGY   (United States)

^c ISTANBUL TECHNICAL UNIVERSITY   (Turkey)

^d Department of Mechanical Engineering ^*  (United States)

^e AIAA   (United States)

^f Aerospace System Design Laboratory   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; FLIGHT CONTROL SYSTEMS; RECONNAISSANCE AIRCRAFT; SPACE SURVEILLANCE;

AUTONOMOUS HOVER CONTROL; FLIGHT MODELING; FLIGHT TESTING;

UNMANNED AERIAL VEHICLES (UAV);

EID: 37249005232     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2007-6818     Document Type: Conference Paper

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