• DocumentCode
    1492133
  • Title

    State feedback ℋ∞-suboptimal control of a rigid spacecraft

  • Author

    Dalsmo, Morten ; Egeland, Olav

  • Author_Institution
    Div. of Eng. Cybern., Norwegian Univ. of Sci. & Technol., Trondheim, Norway
  • Volume
    42
  • Issue
    8
  • fYear
    1997
  • fDate
    8/1/1997 12:00:00 AM
  • Firstpage
    1186
  • Lastpage
    1191
  • Abstract
    A state feedback ℋ∞-suboptimal control problem on TSO(3) for a rigid spacecraft with three control torques and disturbances is addressed, the Hamilton-Jacobi inequality associated with a corresponding state feedback ℋ∞-suboptimal control problem on TS3 is solved globally. The ℋ∞-suboptimal state feedback on TS3 involves the Euler parameters and solves the original problem on TSO(3) when the initial values of the Euler parameters are appropriately chosen
  • Keywords
    H∞ control; Lie groups; aerospace control; matrix algebra; nonlinear systems; space vehicles; state feedback; suboptimal control; Euler parameters; H∞-control; Hamilton-Jacobi inequality; Lie group; TSO(3); nonlinear systems; rigid spacecraft; rotation matrix; state feedback; suboptimal control; Control systems; Cybernetics; Error correction; H infinity control; Nonlinear control systems; Nonlinear systems; Optimal control; Space vehicles; State feedback; Torque control;
  • fLanguage
    English
  • Journal_Title
    Automatic Control, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9286
  • Type

    jour

  • DOI
    10.1109/9.618253
  • Filename
    618253
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=1492133