• DocumentCode
    581661
  • Title

    Adaptive block dynamic surface control of BTT missiles

  • Author

    Mingzhe, Hou ; Haoming, Du ; Feng, Tan ; Canghua, Jiang

  • Author_Institution
    Center for Control Theor. & Guidance Technol., Harbin Inst. of Technol., Harbin, China
  • fYear
    2012
  • fDate
    25-27 July 2012
  • Firstpage
    882
  • Lastpage
    886
  • Abstract
    This paper proposes a novel adaptive block dynamic surface control algorithm for BTT missiles. The control system model of BTT missiles is reconstructed into the block strict-feedback form with matched and unmatched uncertainties. Under the assumption that the uncertainties are norm-bounded, an adaptive block dynamic surface control algorithm is proposed for such a time-varying nonlinear systems. It is proved that the attitude angles can be driven to track the desired trajectory with expected precision and all the states are kept bounded simultaneously by choosing proper design parameters. The simulation results show the effectiveness of the proposed method.
  • Keywords
    adaptive control; aircraft control; feedback; missile control; nonlinear control systems; time-varying systems; uncertain systems; BTT missile; adaptive block dynamic surface control; aircraft control; attitude angle; bank-to-turn technique; block strict-feedback form; design parameters; matched uncertainty; norm-bounded uncertainty; time-varying nonlinear system; trajectory tracking; unmatched uncertainty; Adaptive systems; Aerodynamics; Heuristic algorithms; Missiles; Nonlinear dynamical systems; Uncertainty; Vehicle dynamics; Adaptive Control; BTT Missile; Block Dynamic Surface Control; Nonlinear system;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control Conference (CCC), 2012 31st Chinese
  • Conference_Location
    Hefei
  • ISSN
    1934-1768
  • Print_ISBN
    978-1-4673-2581-3
  • Type

    conf

  • Filename
    6390049