Active fault tolerant control design for reusable launch vehicle using adaptive sliding mode technique

Journal of the Franklin Institute

Volumn 349, Issue 4, 2012, Pages 1543-1560

  Gao, Zhifeng ^a,b   Jiang, Bin ^a   Shi, Peng ^c,d   Qian, Moshu ^a   Lin, Jinxing ^b  

^a NANJING UNIVERSITY OF AERONAUTICS AND ASTRONAUTICS   (China)

^b NANJING UNIVERSITY OF POSTS AND TELECOMMUNICATIONS   (China)

^c UNIVERSITY OF GLAMORGAN   (United Kingdom)

^d VICTORIA UNIVERSITY   (Australia)

Author keywords

[No Author keywords available]

Indexed keywords

ACTIVE FAULT; ACTIVE FAULT TOLERANT CONTROL; ACTUATOR FAULT; ADAPTIVE CONTROL; ADAPTIVE SLIDING MODE; CLOSED-LOOP; DYNAMIC EQUATIONS; FAULT DETECTION SCHEMES; FAULT TOLERANT CONTROL; FLIGHT PHASE; KINEMATIC EQUATIONS; NONLINEAR FAULTS; OUTPUT-TRACKING; REUSABLE LAUNCH VEHICLES; SLIDING MODE TECHNIQUES; SLIDING MODES;

COMMUNICATION SATELLITES; REUSABLE ROCKETS;

REUSABILITY;

EID: 84859162198     PISSN: 00160032     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.jfranklin.2011.11.003     Document Type: Article

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