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On-orbit identification of disturbance torques acting on satellite with rotating payloads

  • Maoliang Chen
  • , Yingying Liu
  • , Jing Lei
  • , Jun Zhou
  • Northwestern Polytechnical University Xian

科研成果: 书/报告/会议事项章节会议稿件同行评审

1 引用 (Scopus)

摘要

This paper presents an approach to improve the stability of three-axis stabilized satellite with rotating payloads from a disturbance identification perspective. Based on steady-state output-only and the system transfer function, the unknown external and internal disturbance torques are identified in a closed loop without persistent excitation. The modified eigensystem identification algorithm(ERA) and the least-squares(LSM) method are employed to obtain the complete models of the disturbance torques. Finally, a feedforward control algorithm is proposed to achieve on-line compensation for the identified disturbance torques. Simulation results show that the approach proposed in this paper can reject the unknown and unwanted disturbance torques effectively, and improve the control performance of satellite with rotating payloads.

源语言英语
主期刊名2009 IEEE International Conference on Mechatronics and Automation, ICMA 2009
1342-1346
页数5
DOI
出版状态已出版 - 2009
活动2009 IEEE International Conference on Mechatronics and Automation, ICMA 2009 - Changchun, 中国
期限: 9 8月 200912 8月 2009

出版系列

姓名2009 IEEE International Conference on Mechatronics and Automation, ICMA 2009

会议

会议2009 IEEE International Conference on Mechatronics and Automation, ICMA 2009
国家/地区中国
Changchun
时期9/08/0912/08/09

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