Robust and adaptive actuator failure compensation designs for a rocket fairing structural-acoustic model

IEEE Transactions on Aerospace and Electronic Systems

Volumn 40, Issue 4, 2004, Pages 1359-1366

  Tang, Xidong ^a   Tao, Gang ^a   Wang, Lingfeng ^a   Stankovic, John A ^a  

^a University of Virginia   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ADAPTIVE CONTROL SYSTEMS; ASYMPTOTIC STABILITY; CLOSED LOOP CONTROL SYSTEMS; CONTROL SYSTEM SYNTHESIS; FAILURE ANALYSIS; MATHEMATICAL MODELS; MICROELECTROMECHANICAL DEVICES; OPTIMAL CONTROL SYSTEMS; ROBUSTNESS (CONTROL SYSTEMS); ROCKETS; SYSTEM STABILITY; VIBRATION CONTROL;

ADAPTIVE ACTUATOR; FAILURE COMPENSATION; ROBUST ACTUATOR; ROCKET FAIRING; STRUCTURAL-ACOUSTIC MODEL;

MICROACTUATORS;

EID: 14744304881     PISSN: 00189251     EISSN: None     Source Type: Journal    
DOI: 10.1109/TAES.2004.1386887     Document Type: Article

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