An adaptive nonlinear output feedback controller using dynamic bounding with an aircraft control application

International Journal of Adaptive Control and Signal Processing

Volumn 23, Issue 7, 2009, Pages 609-639

  Tang, Xidong ^a   Tao, Gang ^b  

^a GM Global RandD Center   (United States)

^b University of Virginia   (United States)

Author keywords

Adaptive control; Aircraft system; Dynamic bounding; Failure compensation; Output feedback

Indexed keywords

ACTUATOR FAILURES; ADAPTIVE BACKSTEPPING CONTROL; ADAPTIVE CONTROL; ADAPTIVE OUTPUT-FEEDBACK CONTROL; AIRCRAFT CONTROL; AIRCRAFT SYSTEM; COMPLETE STABILITY; DYNAMICS UNCERTAINTIES; FAILURE COMPENSATION; FAILURE TIME; LIGHT CONTROL; NON-LINEARITY; NONLINEAR OUTPUT FEEDBACK CONTROLLER; OUTPUT FEEDBACK; PERFORMANCE ANALYSIS; SIMULATION RESULT; STATIC AND DYNAMIC; SYSTEM OUTPUT;

ACTUATORS; ADAPTIVE CONTROL SYSTEMS; AIRCRAFT; BACKSTEPPING; CONTROL NONLINEARITIES; FEEDBACK CONTROL; NONLINEAR SYSTEMS;

FEEDBACK;

EID: 68049124583     PISSN: 08906327     EISSN: 10991115     Source Type: Journal    
DOI: 10.1002/acs.1053     Document Type: Article

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