• DocumentCode
    1702589
  • Title

    Adaptive block dynamic surface control of BTT missiles with input saturations

  • Author

    Hou Mingzhe ; Liang Xiaoling

  • Author_Institution
    Center for Control Theor. & Guidance Technol., Harbin Inst. of Technol., Harbin, China
  • fYear
    2013
  • Firstpage
    915
  • Lastpage
    920
  • Abstract
    An adaptive block dynamic surface control algorithm is proposed for BTT missiles in presence of input saturations. An auxiliary system is introduced, and then the overall system consisting of the auxiliary system and the control system model of the missile is reconstructed into the block strict-feedback form with matched and unmatched uncertainties. By introducing a set of well defined smooth functions to approximate the saturation functions, an adaptive block dynamic surface control algorithm is proposed for this nonlinear system. It is proved that the attitude angles can be driven to track the command signals 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; attitude control; control system synthesis; feedback; missile control; nonlinear control systems; stability; BTT missiles; adaptive block dynamic surface control algorithm; attitude angles; auxiliary system; bank-to-turn missile; block strict-feedback form; command signals; controller design parameters; input saturations; missile control system model; nonlinear system; saturation functions; smooth functions; Aerodynamics; Control systems; Heuristic algorithms; Missiles; Nonlinear dynamical systems; Uncertainty; Vehicle dynamics; Adaptive Control; BTT Missile; Block Dynamic Surface Control; Input saturation; Nonlinear system;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control Conference (CCC), 2013 32nd Chinese
  • Conference_Location
    Xi´an
  • Type

    conf

  • Filename
    6639558