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