• DocumentCode
    313160
  • Title

    Nonlinear singular H suboptimal control for a rigid spacecraft with actuator dynamics

  • Author

    Dalsmo, Morten ; Mass, W.C.A.

  • Author_Institution
    ABB Corp. Res., Vasteras, Sweden
  • Volume
    3
  • fYear
    1997
  • fDate
    4-6 Jun 1997
  • Firstpage
    1879
  • Abstract
    We address a nonlinear singular H suboptimal control problem for a rigid spacecraft with actuator dynamics. Using results from nonlinear H control theory, we find an explicit feedback solution involving the Euler parameters. Our solution is based on a solution to a corresponding nonlinear regular H suboptimal control problem for a rigid spacecraft with three control torques and disturbances
  • Keywords
    H control; aerospace control; dynamics; feedback; nonlinear control systems; space vehicles; suboptimal control; Euler parameters; actuator dynamics; control torques; disturbances; explicit feedback solution; nonlinear singular H suboptimal control; rigid spacecraft; Actuators; Control systems; Earth; Nonlinear systems; Optimal control; Orbits; Space vehicles; State feedback; State-space methods; Torque control;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    American Control Conference, 1997. Proceedings of the 1997
  • Conference_Location
    Albuquerque, NM
  • ISSN
    0743-1619
  • Print_ISBN
    0-7803-3832-4
  • Type

    conf

  • DOI
    10.1109/ACC.1997.610911
  • Filename
    610911