Robust optimal adaptive control method with large adaptive gain

AIAA Infotech at Aerospace Conference and Exhibit and AIAA Unmanned...Unlimited Conference

Volumn , Issue , 2009, Pages

  Nguyen, Nhan T ^a  

^a NASA AMES RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ADAPTIVE CONTROL; ADAPTIVE CONTROL LAW; ADAPTIVE CONTROL METHODS; ADAPTIVE GAIN; ADAPTIVE OPTIMAL CONTROL; FAST ADAPTATIONS; HIGH FREQUENCY OSCILLATIONS; OPTIMAL CONTROL PROBLEM; OPTIMAL CONTROLS; OPTIMALITY CONDITIONS; REFERENCE MODELS; STABILITY ROBUSTNESS; THE STANDARD MODEL; TRACKING ERRORS;

ADAPTIVE CONTROL SYSTEMS; AIRCRAFT CONTROL; CONTROL; DELAY CONTROL SYSTEMS; FLIGHT CONTROL SYSTEMS; GRADIENT METHODS; OPTIMIZATION; ROBUSTNESS (CONTROL SYSTEMS); SYSTEM STABILITY; TRANSPORT AIRCRAFT;

MODEL REFERENCE ADAPTIVE CONTROL;

EID: 77958514640     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (24)

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