DocumentCode :
2853543
Title :
Anti-windup design via nonsmooth multi-objective H optimization
Author :
Biannic, J.-M. ; Apkarian, P.
Author_Institution :
Syst. Control & Flight Dynamics Dept. (DCSD), ONERA, Toulouse, France
fYear :
2011
fDate :
June 29 2011-July 1 2011
Firstpage :
4457
Lastpage :
4462
Abstract :
This paper investigates constrained control design problems involving mixed magnitude and rate saturations. We show that simultaneous design of structured feedback and anti windup gains can be recast as minimizing two H-norm objectives. One is associated with nominal system operation while the other also captures the saturations effects. Because of the two-block structure of the controller, the problem is inherently difficult. We use recently available tools in nonsmooth optimization to compute controller components in a single run thereby alleviating the conservatism of more conventional schemes. The proposed methodology is applied to an aircraft control problem for which a PID feedback controller and a second-order anti-windup compensator are optimized simultaneously.
Keywords :
H control; aircraft control; control system synthesis; feedback; three-term control; H-norm objectives; PID feedback controller; aircraft control; constrained control design; nonsmooth multiobjective H optimization; second-order anti-windup compensator; Actuators; Adaptive control; Aerospace control; Approximation methods; Convergence; Optimization; Robustness; Anti-windup; hinfstruct; magnitude and rate saturations; nonsmooth programming; structured controllers;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference (ACC), 2011
Conference_Location :
San Francisco, CA
ISSN :
0743-1619
Print_ISBN :
978-1-4577-0080-4
Type :
conf
DOI :
10.1109/ACC.2011.5991186
Filename :
5991186
Link To Document :
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