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A novel disturbance observer for attitude control of flexible spacecraft

  • Beihang University
  • Beijing Aerospace Technology Research Institute

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

This paper introduce the high accuracy attitude control method of spacecraft with flexible appendages. It is known that the unwanted vibration modes of flexible appendages will degrade the performance of the flexible spacecraft attitude control system. In this paper, the vibration modes are considered as an 'equivalent' disturbance, and a novel nonlinear disturbance observer is designed to estimate this 'equivalent' disturbance. A disturbance feed-forward compensate controller (DFCC) is designed based on the nonlinear disturbance observer and the feedback linearization control to improve the performance of attitude control system. The flexible spacecraft is controlled by the actuator locate on the central rigid body. Simulation results investigate that the DFCC designed in this paper improved the performance of the attitude control system.

源语言英语
主期刊名Proceedings of the 2016 12th World Congress on Intelligent Control and Automation, WCICA 2016
出版商Institute of Electrical and Electronics Engineers Inc.
297-302
页数6
ISBN(电子版)9781467384148
DOI
出版状态已出版 - 27 9月 2016
活动12th World Congress on Intelligent Control and Automation, WCICA 2016 - Guilin, 中国
期限: 12 6月 201615 6月 2016

出版系列

姓名Proceedings of the World Congress on Intelligent Control and Automation (WCICA)
2016-September

会议

会议12th World Congress on Intelligent Control and Automation, WCICA 2016
国家/地区中国
Guilin
时期12/06/1615/06/16

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