• DocumentCode
    3301631
  • Title

    Active flutter suppression using robust adaptive switching control

  • Author

    Li, Guang ; Dong, Chaoyang ; Hou, Yanze ; Wang, Qing

  • Author_Institution
    Sch. of Autom. Sci. & Electr. Eng., Beijing Univ. of Aeronaut. & Astronaut., Beijing, China
  • fYear
    2009
  • fDate
    15-18 Dec. 2009
  • Firstpage
    782
  • Lastpage
    787
  • Abstract
    Change of aeroservoelastic system dynamics is regarded as the continuous switching of finite models along the flight trajectory or specific flight action, and the switched system is introduced to describe the system dynamics. A robust adaptive switching control scheme is proposed for flutter suppression based on this modeling method. Fast switchings between the models and their corresponding controllers are allowed to cover the aeroservoelastic system dynamics within the flight envelope. In addition, the control scheme avoids the disadvantage of classical adaptive control schemes that system parameters should be slow-varying. Stability of the proposed control scheme is proved by the multiple Lyapunov functions method, and a sufficient condition for stability is achieved. Simulation shows the effectiveness of the proposed scheme.
  • Keywords
    Lyapunov methods; adaptive control; aerospace control; robust control; active flutter suppression; aeroservoelastic system dynamics; continuous switching; finite models; flight action; flight envelope; flight trajectory; multiple Lyapunov functions method; robust adaptive switching control; stability; switched system; Adaptive control; Aerodynamics; Aerospace control; Aircraft; Control systems; Lyapunov method; Programmable control; Robust control; Stability analysis; Switched systems;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Decision and Control, 2009 held jointly with the 2009 28th Chinese Control Conference. CDC/CCC 2009. Proceedings of the 48th IEEE Conference on
  • Conference_Location
    Shanghai
  • ISSN
    0191-2216
  • Print_ISBN
    978-1-4244-3871-6
  • Electronic_ISBN
    0191-2216
  • Type

    conf

  • DOI
    10.1109/CDC.2009.5399970
  • Filename
    5399970