• DocumentCode
    1976663
  • Title

    Adaptive robust attitude tracking control of spacecraft

  • Author

    Motlagh, Reza Banirazi ; Motlagh, M. R Jahed

  • Author_Institution
    Dept. of Electr. Eng., Iran Univ. of Sci. & Technol., Tehran
  • fYear
    2005
  • fDate
    28-31 Aug. 2005
  • Firstpage
    498
  • Lastpage
    503
  • Abstract
    A nonlinear adaptive-robust scheme is presented to control a class of nonlinear systems. It effectively combines the design techniques of adaptive and robust control to improve performance by retaining the advantages of both techniques. It enhances transient performance and eliminates robustness problems compared to a parameter adaptive control. It also improves tracking performance by reducing modeling uncertainty and optimizes control effort by estimating bound uncertainty compared to a deterministic robust control. The controller is applied to a spacecraft making the body frame track a reference orientation, when there are parametric uncertainty, modeling errors, and external disturbances
  • Keywords
    adaptive control; attitude control; control system synthesis; nonlinear control systems; robust control; space vehicles; tracking; uncertain systems; deterministic robust control; external disturbance; modeling error; nonlinear adaptive-robust scheme; nonlinear system control; optimal control; parametric uncertainty; reference orientation; spacecraft adaptive robust attitude tracking control; transient performance; uncertainty modeling; Adaptive control; Attitude control; Control systems; Error correction; Nonlinear control systems; Nonlinear systems; Programmable control; Robust control; Space vehicles; Uncertainty;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control Applications, 2005. CCA 2005. Proceedings of 2005 IEEE Conference on
  • Conference_Location
    Toronto, Ont.
  • Print_ISBN
    0-7803-9354-6
  • Type

    conf

  • DOI
    10.1109/CCA.2005.1507175
  • Filename
    1507175