• 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