Propulsion control of crippled aircraft by H ∞ model matching

IEEE Transactions on Control Systems Technology

Volumn 7, Issue 2, 1999, Pages 142-159

  Jonckheere, Edmond A ^a,b   Yu, Gwo Ruey ^c  

^a IEEE   (United States)

^b University of Southern California   (United States)

^c I SHOU UNIVERSITY   (Taiwan)

Author keywords

Aircraft control; Aircraft propulsion; Aircraft reliability; Control; H infinity; Human factors; Model reference adaptive control; Reconfigurable architecture; Robustness

Indexed keywords

ADAPTIVE CONTROL SYSTEMS; AIRCRAFT PROPULSION; COMPUTER SIMULATION; CONTROL SYSTEM ANALYSIS; CONTROL SYSTEM SYNTHESIS; CONTROLLABILITY; FAILURE ANALYSIS; MATHEMATICAL MODELS; MOTION CONTROL; ROBUSTNESS (CONTROL SYSTEMS);

PROPULSION CONTROLLED AIRCRAFT (PCA) DESIGN; SYNTHESIZE MODEL MATCHING;

OPTIMAL CONTROL SYSTEMS;

EID: 0033098885     PISSN: 10636536     EISSN: None     Source Type: Journal    
DOI: 10.1109/87.748142     Document Type: Article

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