• DocumentCode
    1751587
  • Title

    A velocity-based framework for the robust stability analysis of dynamic inversion flight controllers

  • Author

    Tsourdos, A. ; Leith, D.J. ; Leithead, W.E. ; White, B.A.

  • Author_Institution
    Dept. of Aerospace, Power & Sensors, Cranfield Univ.-RMCS, UK
  • Volume
    5
  • fYear
    2001
  • fDate
    2001
  • Firstpage
    3341
  • Abstract
    Methods for analysing the robustness of linear systems to parametric uncertainty are relatively well developed. However, the converse is true for nonlinear systems. The recently developed velocity-based framework provides a degree of continuity with linear methods which has the potential to allow established linear methods to be applied when analysing the robustness of nonlinear systems to uncertainty. This paper reports initial investigations in this area with particular reference to the guided weapons application area
  • Keywords
    control system analysis; missile guidance; nonlinear control systems; robust control; uncertain systems; dynamic inversion flight controllers; guided missiles; guided weapons; nonlinear systems; parametric uncertainty; robust stability analysis; robustness analysis; velocity-based framework; Aerodynamics; Linear systems; Nonlinear dynamical systems; Nonlinear systems; Robust control; Robust stability; Robustness; Uncertainty; Vehicle dynamics; Velocity control;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    American Control Conference, 2001. Proceedings of the 2001
  • Conference_Location
    Arlington, VA
  • ISSN
    0743-1619
  • Print_ISBN
    0-7803-6495-3
  • Type

    conf

  • DOI
    10.1109/ACC.2001.946144
  • Filename
    946144