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Early warning satellite attitude SMC base on ESO

  • Beihang University

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

A novel approach combining the sliding mode control (SMC) and extended state observer (ESO) is proposed for attitude control of an early warning satellite model which is non-linear in dynamics. The sliding mode controller is designed to guarantee the state variables of the closed-loop system to converge to the reference state with the help of the ESO by estimating the unknown disturbance. Then, simulation results illustrate the effectiveness of the control strategy.

源语言英语
主期刊名2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014
出版商Institute of Electrical and Electronics Engineers Inc.
1589-1594
页数6
ISBN(电子版)9781479946990
DOI
出版状态已出版 - 12 1月 2015
活动6th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014 - Yantai, 中国
期限: 8 8月 201410 8月 2014

出版系列

姓名2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014

会议

会议6th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014
国家/地区中国
Yantai
时期8/08/1410/08/14

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