• DocumentCode
    391058
  • Title

    A LPV approach to robust H2 and H static output-feedback design

  • Author

    Shaked, U.

  • Author_Institution
    Dept. of Electr. Eng.-Syst., Tel Aviv Univ., Israel
  • Volume
    3
  • fYear
    2002
  • fDate
    10-13 Dec. 2002
  • Firstpage
    3476
  • Abstract
    A linear parameter varying approach for designing a constant output feedback controller for a linear time-invariant system with uncertain parameters that achieves a minimum bound on either the H2 or the H performance level is introduced. Assuming that the uncertain parameters reside in a given polytope a parameter dependent Lyapunov function is described which enables the derivation of the required constant gain via a solution of a set of linear matrix inequalities that correspond to the vertices of the uncertainty polytope.
  • Keywords
    H control; Lyapunov methods; aircraft control; control system synthesis; feedback; linear matrix inequalities; linear systems; military aircraft; robust control; uncertain systems; LPV approach; linear matrix inequalities; linear parameter varying approach; linear time-invariant system; minimum bound; parameter dependent Lyapunov function; polytopic uncertainty; robust H static output-feedback design; robust H2 static output-feedback design; uncertain parameters; Bandwidth; Control systems; Linear matrix inequalities; Lyapunov method; Open loop systems; Output feedback; Robustness; Sufficient conditions; Uncertainty; Vectors;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Decision and Control, 2002, Proceedings of the 41st IEEE Conference on
  • ISSN
    0191-2216
  • Print_ISBN
    0-7803-7516-5
  • Type

    conf

  • DOI
    10.1109/CDC.2002.1184413
  • Filename
    1184413