117 / 2016-04-28 11:21:38
Finite Time Sliding Mode Controller for a rigid Satellite in Presence of Actuator Failure
satellite attitude control,finite time sliding mode control
全文录用
Hamed Yadegari / Beihang University (Buaa)
Chao Han / Beihang University (Buaa)
Yukai Zhu / Beihang University (Buaa)
Attitude control executes an important role in satellite performance and is one of most critical implement in development of spacecraft technology. According to the presence of several uncertainties and disturbances in complicated satellite system in harsh space environment, taking advantage of developed anti-disturbance control methods is beneficial. This paper presents some nonlinear sliding mode control scheme for a satellite with various reaction wheel faults as uncertain parameters. Attitude quaternion and its derivative commands are robustly tracked via sliding mode controllers to become inclined to zero.
重要日期
  • 会议日期

    07月08日

    2016

    07月10日

    2016

  • 04月25日 2016

    终稿截稿日期

  • 05月20日 2016

    初稿截稿日期

  • 07月10日 2016

    注册截止日期

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