• DocumentCode
    2848849
  • Title

    A parameter-dependent performance criterion for linear parameter-varying systems

  • Author

    Lee, Lawton H. ; Spillman, Mark

  • Author_Institution
    Lockheed Martin Missiles & Space, Sunnyvale, CA, USA
  • Volume
    2
  • fYear
    1997
  • fDate
    10-12 Dec 1997
  • Firstpage
    984
  • Abstract
    Existing control theory for linear parameter-varying systems uses a uniform-in-the-parameters upper bound (a constant scalar) on the induced-L2 norm. In this paper, this constant is generalized to a function of the parameters; the performance criterion generalizes to an integral quadratic constraint and implies a norm bound that depends naturally on the real-time parameter trajectory. As in existing theory, the synthesis problem reduces to convex optimization involving linear matrix inequalities. A motivating example, gain-scheduled flight control of the F-16 VISTA, demonstrates the flexibility gained by incorporating the new performance criterion
  • Keywords
    control system synthesis; matrix algebra; optimal control; performance index; time-varying systems; F-16 VISTA; LMI; control synthesis; convex optimization; gain-scheduled flight control; induced-L2 norm; integral quadratic constraint; linear matrix inequalities; linear parameter-varying systems; parameter-dependent performance criterion; real-time parameter trajectory; uniform-in-the-parameters upper bound; Aerospace control; Control theory; Dynamic scheduling; Ear; Linear matrix inequalities; Missiles; Nonlinear control systems; Performance analysis; Time varying systems; Upper bound;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Decision and Control, 1997., Proceedings of the 36th IEEE Conference on
  • Conference_Location
    San Diego, CA
  • ISSN
    0191-2216
  • Print_ISBN
    0-7803-4187-2
  • Type

    conf

  • DOI
    10.1109/CDC.1997.657572
  • Filename
    657572