Adaptive compensation of aircraft actuation failures using an engine differential model

IEEE Transactions on Control Systems Technology

Volumn 16, Issue 5, 2008, Pages 971-982

  Liu, Yu ^a   Tang, Xidong ^a   Tao, Gang ^a,b   Joshi, Suresh M ^c  

^a University of Virginia   (United States)

^b GENERAL MOTORS CORPORATION   (United States)

^c NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

Actuator failures; Adaptive compensation; Aircraft control; Engine differentials; Tracking

Indexed keywords

ACTUATORS; AIRCRAFT MODELS; FLIGHT DYNAMICS; TRANSPORT AIRCRAFT;

ACTUATOR FAILURES; ADAPTIVE COMPENSATION; AILERON FAILURES; AIRCRAFT CONTROL; AIRCRAFT FLIGHT CONTROL; AIRCRAFT FLIGHT DYNAMICS; ASYMPTOTIC TRACKING; CONTROL SCHEMES; DIFFERENTIAL MODELS; DIFFERENTIAL-MODE; DIRECT ADAPTIVE CONTROL; ENGINE DIFFERENTIALS; FAILURE COMPENSATION; LATERAL MOTIONS; NONLINEAR AIRCRAFT MODEL; SIMULATION RESULTS; TRACKING;

AIRCRAFT;

EID: 49249119714     PISSN: 10636536     EISSN: None     Source Type: Journal    
DOI: 10.1109/TCST.2007.906273     Document Type: Article

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