• DocumentCode
    637765
  • Title

    Altitude control of a satellite using a feedback linearization

  • Author

    Benenia, M. ; Batatia, H. ; Camino, F. Mora ; Benslama, M.

  • Author_Institution
    Electromagn. & Telecommun. Lab., Constantine Univ., Constantine, Algeria
  • fYear
    2013
  • fDate
    4-5 June 2013
  • Firstpage
    1
  • Lastpage
    6
  • Abstract
    This study is dedicated to the problem of non linear attitude control for a rigid large angle maneuver satellite. The non linear control method is based upon the linearization of the input-output of the system, also called feedback linearization, via state feedback. The output function is chosen amongst the attitude quaternion parameters.
  • Keywords
    artificial satellites; attitude control; state feedback; altitude control; attitude quaternion parameters; feedback linearization; nonlinear attitude control; rigid large angle maneuver satellite; state feedback; feedback linearization; quaternion; sliding mode control; spacecraft attitude control;
  • fLanguage
    English
  • Publisher
    iet
  • Conference_Titel
    Control and Automation 2013: Uniting Problems and Solutions, IET Conference on
  • Conference_Location
    Birmingham
  • Electronic_ISBN
    978-1-84919-710-6
  • Type

    conf

  • DOI
    10.1049/cp.2013.0018
  • Filename
    6613731
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=637765