• DocumentCode
    3069949
  • Title

    Application of improved L2-gain synthesis on LPV missile autopilot design

  • Author

    Lim, Sungyung ; How, Jonathan P.

  • Author_Institution
    Dept. of Aeronaut. & Astronaut., Stanford Univ., CA, USA
  • Volume
    6
  • fYear
    1999
  • fDate
    1999
  • Firstpage
    3733
  • Abstract
    Presents an improved finite-dimensional linear matrix inequality (LMI) formulation for the L2-gain synthesis of a piecewise-affine linear parameter-varying (PALPV) system. The new formulation is then used to design a missile autopilot to investigate issues such as the effectiveness, reliability, and conservatism. Our approach is based on a nonsmooth dissipative systems framework using a continuous, quasi-piecewise-affine parameter-dependent Lyapunov function (QPAL) which has been shown to yield a less conservative, guaranteed result than previously published techniques based on quasi-affine parameter-dependent Lyapunov functions (QALs) or Lure-Postnikov Lyapunov functions. The results in the paper improve the computational efficiency by using a different “convexifying” technique. We also generalize our previous results by eliminating the restriction on the number of parameters
  • Keywords
    Lyapunov methods; closed loop systems; control system synthesis; linear systems; matrix algebra; missile control; robust control; L2-gain synthesis; computational efficiency; continuous quasi-piecewise-affine parameter-dependent Lyapunov function; convexifying technique; finite-dimensional linear matrix inequality formulation; missile autopilot; nonsmooth dissipative systems; piecewise-affine linear parameter-varying system; Aerodynamics; Computational efficiency; Control system synthesis; Guidelines; Linear systems; Lyapunov method; Missiles; Process design; Signal synthesis; Time varying systems;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    American Control Conference, 1999. Proceedings of the 1999
  • Conference_Location
    San Diego, CA
  • ISSN
    0743-1619
  • Print_ISBN
    0-7803-4990-3
  • Type

    conf

  • DOI
    10.1109/ACC.1999.786188
  • Filename
    786188