DocumentCode :
1805220
Title :
A hybrid LQR/LP approach for addressing actuator saturation in feedback control
Author :
Chandler, P.R. ; Mears, M.J. ; Pachter, M.
Author_Institution :
WL/FIG, Wright-Patterson AFB, OH, USA
Volume :
4
fYear :
1994
fDate :
14-16 Dec 1994
Firstpage :
3860
Abstract :
A hybrid optimization approach is advanced for mitigating actuator saturation effects in model following feedback control as applied to adaptive and reconfigurable flight control systems. The linear quadratic regulator and linear programming paradigms are combined such that a suboptimal tracking control law that does not violate the control constraints can be synthesized in real time
Keywords :
aircraft control; control system synthesis; feedback; linear programming; linear quadratic control; model reference adaptive control systems; actuator saturation effects mitigation; adaptive reconfigurable flight control systems; control law synthesis; feedback control; hybrid LQR/LP approach; hybrid optimization approach; linear programming; linear quadratic regulator; model-following feedback control; suboptimal tracking control law; Actuators; Adaptive control; Aerospace control; Cost function; Degradation; Feedback control; Optimal control; Programmable control; Regulators; Tracking loops;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Decision and Control, 1994., Proceedings of the 33rd IEEE Conference on
Conference_Location :
Lake Buena Vista, FL
Print_ISBN :
0-7803-1968-0
Type :
conf
DOI :
10.1109/CDC.1994.411771
Filename :
411771
Link To Document :
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