Adaptive actuator nonlinearity compensation and disturbance rejection applied to aircraft models with synthetic jet actuators

AIAA Guidance, Navigation, and Control Conference

Volumn , Issue , 2010, Pages

  Mondschein, Stephen T ^a   Tao, Gang ^a   Burkholder, Jason O ^b  

^a University of Virginia   (United States)

^b Barron Associates Inc   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATOR NONLINEARITIES; ADAPTIVE ACTUATOR; ADAPTIVE APPROACH; ADAPTIVE DISTURBANCE REJECTION; ADAPTIVE INVERSE; CONTROL SYSTEM MODELS; FEEDBACK CONTROL LAW; LINEAR TIME INVARIANT SYSTEMS; NOMINAL SYSTEM; SYNTHETIC JET ACTUATORS; UNKNOWN PARAMETERS;

AIRCRAFT MODELS; CONTROL THEORY; FLIGHT CONTROL SYSTEMS;

ACTUATORS;

EID: 84867807495     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2010-8149     Document Type: Conference Paper

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