NDLI: Anti-windup design via nonsmooth multi-objective H∞ optimization

Content Provider	IEEE Xplore Digital Library
Author	Biannic, J.-M. Apkarian, P.
Copyright Year	2011
Description	Author affiliation: Syst. Control & Flight Dynamics Dept. (DCSD), ONERA, Toulouse, France (Biannic, J.-M.; Apkarian, P.)
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.
Sponsorship	Control Syst. Soc.
Starting Page	4457
Ending Page	4462
File Size	290311
Page Count	6
File Format	PDF
ISBN	9781457700804
ISSN	07431619
e-ISBN	9781457700811
DOI	10.1109/ACC.2011.5991186
Language	English
Publisher	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Publisher Date	2011-06-29
Publisher Place	USA
Access Restriction	Subscribed
Rights Holder	American Automatic Control Council(AACC)
Subject Keyword	Optimization Approximation methods Adaptive control Robustness Convergence Aerospace control Actuators nonsmooth programming Anti-windup magnitude and rate saturations structured controllers hinfstruct
Content Type	Text
Resource Type	Article
Subject	Electrical and Electronic Engineering

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