• DocumentCode
    2085822
  • Title

    Online nonlinear guaranteed estimation with application to a high performance aircraft

  • Author

    Scholte, Eelco ; Campbell, Mark E.

  • Author_Institution
    Depaxtment of Mech. & Aerosp. Eng., Cornell Univ., Ithaca, NY, USA
  • Volume
    1
  • fYear
    2002
  • fDate
    2002
  • Firstpage
    184
  • Abstract
    The most commonly used filters (or estimators) for online control customization are based upon stochastic assumptions on the noise. In this paper a set-membership filter is extended to be used with nonlinear systems for which the Jacobian and Hessian are continuous over the uncertainty interval. This filter relies on assuming that the noise sources are bounded in order to obtain hard bounds on state and parameter estimates. These bounds are then compatible with robust control design so that the controller can be adequately updated in real-time. The method proposed is referred to as an extended set-membership filter and is applied to a two-state example and to the state and parameter estimations of a complex F-15 like model.
  • Keywords
    aircraft control; military aircraft; nonlinear systems; parameter estimation; real-time systems; robust control; state estimation; high performance aircraft; military aircraft; nonlinear guaranteed estimation; nonlinear systems; parameter estimation; real time control; robust control; set-membership filter; state estimation; Aerospace control; Aircraft propulsion; Filters; Missiles; Nonlinear systems; Parameter estimation; Robust control; State estimation; Stochastic resonance; Uncertainty;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    American Control Conference, 2002. Proceedings of the 2002
  • ISSN
    0743-1619
  • Print_ISBN
    0-7803-7298-0
  • Type

    conf

  • DOI
    10.1109/ACC.2002.1024801
  • Filename
    1024801