• DocumentCode
    2856925
  • Title

    State feedback H∞ control of a rigid spacecraft

  • Author

    Dalsmo, Morten ; Egeland, Olav

  • Author_Institution
    Div. of Eng. Cybern., Norwegian Inst. of Technol., Trondheim, Norway
  • Volume
    4
  • fYear
    1995
  • fDate
    13-15 Dec 1995
  • Firstpage
    3968
  • Abstract
    In the present paper we address a state feedback H∞ suboptimal control problem for a rigid spacecraft with three control torques and disturbances. The state feedback H∞ suboptimal control problem on TSO(3) is transferred to a corresponding state feedback H∞ suboptimal control problem on TS3, and the Hamilton-Jacobi inequality associated with this problem is solved. We obtain a state feedback control law involving the Euler parameters which solves the problem formulated on TS3 globally. This state feedback also solves the original problem on TSO(3) when the initial values of the Euler parameters are appropriately chosen
  • Keywords
    H∞ control; Jacobian matrices; aerospace control; space vehicles; state feedback; suboptimal control; Euler parameters; Hamilton-Jacobi inequality; TS3; TSO(3); control torques; disturbances; rigid spacecraft; state feedback H∞ suboptimal control problem; Closed loop systems; Control systems; H infinity control; Nonlinear control systems; Nonlinear systems; Optimal control; Space vehicles; State feedback; State-space methods; Torque control;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Decision and Control, 1995., Proceedings of the 34th IEEE Conference on
  • Conference_Location
    New Orleans, LA
  • ISSN
    0191-2216
  • Print_ISBN
    0-7803-2685-7
  • Type

    conf

  • DOI
    10.1109/CDC.1995.479224
  • Filename
    479224
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=2856925