Intelligent fuzzy variable structure control of flexible spacecraft

Yanan Yu*, Xiuyun Meng, Keyong Li

*此作品的通讯作者

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

Aiming at the problem of vibration suppression of flexible spacecraft and high frequency chattering of sliding mode variable structure control torque, a real-time optimization sliding mode variable structure control algorithm based on the intelligent fuzzy method is proposed. Through designing variable structure control strategy with exponential approach law, the spacecraft attitude control and vibration suppression of flexible appendages are achieved. However, the control torque may present high frequency chattering during the sliding phase, and effect of vibration suppression will be weakened. The intelligent fuzzy control algorithm is used to eliminate chattering by optimizing parameters of the control system. Numerical simulations show that the high frequency chattering of control torque is restrained effectively and vibration suppression can be accomplished with faster convergence.

源语言英语
主期刊名2011 International Conference on Electrical and Control Engineering, ICECE 2011 - Proceedings
4814-4817
页数4
DOI
出版状态已出版 - 2011
活动2nd Annual Conference on Electrical and Control Engineering, ICECE 2011 - Yichang, 中国
期限: 16 9月 201118 9月 2011

出版系列

姓名2011 International Conference on Electrical and Control Engineering, ICECE 2011 - Proceedings

会议

会议2nd Annual Conference on Electrical and Control Engineering, ICECE 2011
国家/地区中国
Yichang
时期16/09/1118/09/11

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