• DocumentCode
    282370
  • Title

    Output variable structure control of the longitudinal motion of an aircraft

  • Author

    White, B.A.

  • Author_Institution
    R. Mil. Coll. of Sci., Shrivenham, UK
  • fYear
    1989
  • fDate
    32841
  • Firstpage
    42461
  • Lastpage
    42464
  • Abstract
    A variable structure control system (VSCS) essentially tries to keep the dynamic behaviour of a system constant by dynamically varying the feedback gains of the system. Two compensator blocks contain gains that the VSCS switches dynamically in order to maintain the performance of the closed loop system. The switching is controlled by reference to a performance measure or switching function that is constructed from either the state vector or the output vector of the system. This performance measure is used in a switching strategy to minimise the deviation of the system performance away from the desired performance. The output from the performance measure is zero when the system is performing correctly, and the switching strategy is designed to maintain the performance measure at zero at all times. As an example of VSCS, the control of the longitudinal motion of an aircraft is considered
  • Keywords
    aircraft control; attitude control; closed loop systems; variable structure systems; aircraft control; attitude control; dynamic behaviour; longitudinal motion; switching strategy; variable structure control system;
  • fLanguage
    English
  • Publisher
    iet
  • Conference_Titel
    Navigation, Guidance and Control on Aerospace, IEE Colloquium on
  • Conference_Location
    London
  • Type

    conf

  • Filename
    199074