• DocumentCode
    490072
  • Title

    Sliding-Mode Controller Design for Spacecraft Attitude Tracking Maneuvers

  • Author

    Chen, Yon-Ping ; Lo, Shih-Che

  • Author_Institution
    Institute of Control Engineering, National Chiao Tung University, Hsinchu, Taiwan 30039, R.O.C
  • fYear
    1993
  • fDate
    2-4 June 1993
  • Firstpage
    195
  • Lastpage
    196
  • Abstract
    This paper presents a robust sliding-mode control law to deal with the spacecraft attitude tracking problems. Two important natural properties related to the spacecraft model of motion are shown and then by using these properties and the second method of Lyapunov thoery, the system stability in the sliding mode can be easily achieved.
  • Keywords
    Attitude control; Control engineering; Equations; Kinematics; Lyapunov method; Robust control; Sliding mode control; Space vehicles; Stability analysis; Symmetric matrices;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    American Control Conference, 1993
  • Conference_Location
    San Francisco, CA, USA
  • Print_ISBN
    0-7803-0860-3
  • Type

    conf

  • Filename
    4792835
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=490072