Adaptive control for a nonlinear wing section with multiple flaps

Journal of Guidance, Control, and Dynamics

Volumn 29, Issue 3, 2006, Pages 744-749

  Behal, A ^a,b,c   Rao, V M ^a   Marzocca, P ^a,b,c   Kamaludeen, M ^a  

^a CLARKSON UNIVERSITY   (United States)

^b Department of Electrical and Computer Engineering ^*

^c AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; FEEDBACK; NONLINEAR SYSTEMS; OSCILLATIONS; ROBUSTNESS (CONTROL SYSTEMS); WINGS;

FLIGHT SPEED; FLUTTER BOUNDARY; LIMIT CYCLE OSCILLATIONS (LCO);

ADAPTIVE CONTROL SYSTEMS;

EID: 33744731453     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/1.18182     Document Type: Article

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