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Sampled-data H control for attitude stabilization and vibration suppression of flexible spacecrafts

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 develops a sampled-data H control strategy for attitude stabilization and vibration suppression of flexible spacecrafts. After introducing an impulsive observer-based sampled-data controller, the closed-loop system is built as a type of hybrid systems consisting a continuous-time and an impulsive differential system. Based on Lyapunov functional method, a sufficient condition is derived such that the closed-loop system is asymptotic stable and satisfies a prescribed H performance. The minimum attenuation level and desired controller parameters can be obtained by solving a convex optimization problem involving linear matrix inequalities (LMIs). An illustrative design example proves the effectiveness of the developed sampled-data control strategy.

源语言英语
主期刊名Proceedings of the 36th Chinese Control Conference, CCC 2017
编辑Tao Liu, Qianchuan Zhao
出版商IEEE Computer Society
6376-6381
页数6
ISBN(电子版)9789881563934
DOI
出版状态已出版 - 7 9月 2017
已对外发布
活动36th Chinese Control Conference, CCC 2017 - Dalian, 中国
期限: 26 7月 201728 7月 2017

出版系列

姓名Chinese Control Conference, CCC
ISSN(印刷版)1934-1768
ISSN(电子版)2161-2927

会议

会议36th Chinese Control Conference, CCC 2017
国家/地区中国
Dalian
时期26/07/1728/07/17

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