• DocumentCode
    486547
  • Title

    Reachable Outputs in Systems with Bounded Parameter Uncertainties: Application to Failure Detection

  • Author

    Horak, Dan T. ; Goblirsch, David M.

  • Author_Institution
    Bendix Aerospace Technology Center, 9140 Old Annapolis Road, Columbia, Maryland 21045
  • fYear
    1986
  • fDate
    18-20 June 1986
  • Firstpage
    301
  • Lastpage
    308
  • Abstract
    A method for computing the intervals in which the outputs of a linear multivariable dynamic system with bounded parameter uncertainties and noise must lie has been developed. It utilizes Pontryagin´s Maximum Principle and is recursive. Because of its computational efficiency it can be executed in real time and used for system and sensor failure detection in systems with parameter uncertainties. Failures are detected by testing if the measured outputs lie outside the computed intervals, indicating that the system cannot be described by the given model and the specified parameter uncertainty bounds. The method is illustrated by application to the longitudinal dynamics of the AFTI F-16 aircraft.
  • Keywords
    Aerodynamics; Aerospace control; Aircraft navigation; Computational efficiency; Condition monitoring; Power system modeling; Real time systems; Robustness; Uncertain systems; Uncertainty;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    American Control Conference, 1986
  • Conference_Location
    Seattle, WA, USA
  • Type

    conf

  • Filename
    4788952