DocumentCode :
3420244
Title :
Adaptive actuator failure compensation for a transport aircraft model
Author :
Chen, Shuhao ; Tao, Gang ; Joshi, Suresh M.
Author_Institution :
Dept. of Electr. & Comput. Eng., Virginia Univ., Charlottesville, VA, USA
Volume :
3
fYear :
2001
fDate :
2001
Firstpage :
1827
Abstract :
Adaptive actuator failure compensation schemes are developed for a class of multi-input and single-output plants with actuator failures characterized by certain inputs stuck at some unknown fixed value at unknown time instants. Conditions and controller structures for achieving state tracking and output tracking in the presence of actuator failures are derived. Adaptive laws are designed for updating some of the controller parameters when the actuator failure parameters are unknown. Simulation results for a linearized transport aircraft model with actuator failure show the desired system performance with adaptive failure compensation
Keywords :
actuators; adaptive control; aircraft control; compensation; linearisation techniques; multivariable control systems; uncertain systems; MISO plants; adaptive actuator failure compensation; linearized transport aircraft model; output tracking; state tracking; transport aircraft model; Adaptive control; Aerospace control; Aircraft propulsion; Control systems; Ear; Hydraulic actuators; NASA; Postal services; Programmable control; State feedback;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference, 2001. Proceedings of the 2001
Conference_Location :
Arlington, VA
ISSN :
0743-1619
Print_ISBN :
0-7803-6495-3
Type :
conf
DOI :
10.1109/ACC.2001.946001
Filename :
946001
Link To Document :
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