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Attitude coordination control of spacecraft formation

  • 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

摘要

In this paper, we study adaptive attitude synchronization of spacecraft formation with switching topology. By introducing a novel adaptive control architecture and by transforming the attitude dynamics into Euler-Lagrange form, decentralized controllers are developed, which allow for parametric uncertainties and unknown external disturbances. Based upon graph theory and Lyapunov stability theory, rigid mathematical analysis on system stability is provided. A distinctive feature of this work is to address the adaptive attitude synchronization with general directed information flow. It is shown that arbitrary desired constant relative orientations within the group or with respect to any external references can be attained. Simulation results are provided to demonstrate the effectiveness of the obtained results.

源语言英语
主期刊名Information Technology Applications in Industry
795-802
页数8
版本PART 1
DOI
出版状态已出版 - 2013
活动2012 International Conference on Information Technology and Management Innovation, ICITMI 2012 - Guangzhou, 中国
期限: 10 11月 201211 11月 2012

丛书

姓名Applied Mechanics and Materials
编号PART 1
263-266
ISSN(印刷版)1660-9336
ISSN(电子版)1662-7482

会议

会议2012 International Conference on Information Technology and Management Innovation, ICITMI 2012
国家/地区中国
Guangzhou
时期10/11/1211/11/12

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