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
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