Identification of a UAV and design of a hardware-in-the-loop system, for nonlinear control purposes

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

Volumn 8, Issue , 2005, Pages 6441-6446

  Manaï, Myriam ^a,c,d   Desbiens, André ^a,c,d   Gagnon, Eric ^b,d,e  

^a UNIVERSITÉ LAVAL   (Canada)

^b DEFENCE RESEARCH AND DEVELOPMENT CANADA VALCARTIER   (Canada)

^c Pavilion Adrien Pouliot ^*  (Canada)

^d AIAA   (United States)

^e Precision Weapons Section   (Canada)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; FLIGHT DYNAMICS; MATHEMATICAL MODELS; PROCESS CONTROL; SYSTEMS ANALYSIS; TEST FACILITIES; UNMANNED VEHICLES;

LOOP SYSTEMS; MODEL PARAMETERS; OUTPUT-ERROR APPROACH ALGORITHMS; UAV AUTOPILOT;

NONLINEAR CONTROL SYSTEMS;

EID: 29744454538     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2005-6483     Document Type: Conference Paper

References (10)

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10. Hoak, D. E. and Finck, R. F., USAF Stability and Control Datcom, Flight Control Division, Air Force Flight Dynamics Laboratory, Wright-Patterson Air Force Base, Ohio, April 1978.