Adaptive linear quadratic design with application to F-16 fighter aircraft

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

Volumn 5, Issue , 2004, Pages 3427-3435

  Huo, Ying ^a,d   Mirmirani, Majdedin ^b,d   Ioannou, Petros ^a,d   Colgren, Richard ^c,d  

^a UNIVERSITY OF SOUTHERN CALIFORNIA   (United States)

^b CALIFORNIA STATE UNIVERSITY   (United States)

^c UNIVERSITY OF KANSAS   (United States)

^d Dept of Electrical Engineering ^*  (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; COMPUTER SIMULATION; CONTROL SYSTEMS; FAULT TOLERANT COMPUTER SYSTEMS; LINEAR SYSTEMS; MATHEMATICAL MODELS; SCHEDULING;

ADAPTIVE LINEAR QUADRATIC (ALQ) CONTROL; AIRCRAFT DYNAMICS; GAIN SCHEDULING; LINEAR QUADRATIC (LQ) CONTROL;

FIGHTER AIRCRAFT;

EID: 19944412187     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2004-5421     Document Type: Conference Paper

References (12)

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