Modified adaptive fault diagnosis method and its application to flight control systems

Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica

Volumn 30, Issue 7, 2009, Pages 1271-1276

  Zhang, Ke ^a   Jiang, Bin ^a  

^a NANJING UNIVERSITY OF AERONAUTICS AND ASTRONAUTICS   (China)

Author keywords

Adaptive observer; Fault diagnosis; Fault estimation; Flight dynamics; Linear matrix inequalities

Indexed keywords

ADAPTIVE OBSERVER; DESIGN METHOD; ERROR DYNAMICS; FAULT DIAGNOSIS; FAULT DIAGNOSIS METHOD; FAULT ESTIMATION; LYAPUNOV STABILITY THEORY; MATRIX INEQUALITY; PERFORMANCE REQUIREMENTS; SIMULATION RESULT; SUFFICIENT CONDITIONS;

ADAPTIVE CONTROL SYSTEMS; DESIGN; DYNAMICAL SYSTEMS; ESTIMATION; FAILURE ANALYSIS; FLIGHT DYNAMICS; LINEAR CONTROL SYSTEMS; LINEAR MATRIX INEQUALITIES; OBSERVABILITY; SWITCHING SYSTEMS; SYSTEM STABILITY;

FLIGHT CONTROL SYSTEMS;

EID: 68549136579     PISSN: 10006893     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

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