• DocumentCode
    3215615
  • Title

    Attitude Control of Missile with Time-delay

  • Author

    Yupeng Qiao ; Daizhan Cheng

  • Author_Institution
    Acad. of Math. & Syst. Sci., Chinese Acad. of Sci., Beijing, China
  • fYear
    2006
  • fDate
    7-11 Aug. 2006
  • Firstpage
    267
  • Lastpage
    272
  • Abstract
    In this paper the Fliess expansion is used for attitude control of missile to consider the case when the control is piecewise. In practice, the control can only be realized with two modifications: (i) instead of "rectangle controls" we can only have "trapezoid controls"; (ii) the controls must have certain time delay. In this paper the tracking problem via delayed trapezoid controls is considered. The theoretical results are applied to the attitude control of missiles.
  • Keywords
    attitude control; delays; missile control; piecewise linear techniques; tracking; Fliess functional expansion; attitude control; delayed trapezoid controls; missile; rectangle controls; time delay tracking control; Bang-bang control; Control systems; Delay effects; Friction; Mathematics; Missiles; Nonlinear control systems; Predictive models; Robust control; Uncertainty; Attitude control of missile; Fliess functional expansion; time-delay tracking control;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control Conference, 2006. CCC 2006. Chinese
  • Conference_Location
    Harbin
  • Print_ISBN
    7-81077-802-1
  • Type

    conf

  • DOI
    10.1109/CHICC.2006.280966
  • Filename
    4060514
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=3215615