A variable structure attitude control system design based on finite time stability

Rui Min Jiang, Jun Zhou, Jian Guo Guo

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

A variable structure attitude control system design method that guarantees the finite-time stability is proposed for hypersonic vehicle attitude control. According to the characteristics of the hypersonic vehicle longitudinal attitude model, it is considered to comprise attack angle control loop and angular rate control loop. The attack angle controller and pitch angular rate controller based on variable structure control are designed respectively which ensure the finite-time stability. The finite-time stability of the whole attitude control system has been proved.The simulation results illustrated that the proposed attitude controller has good rapidity and robustness.

源语言英语
主期刊名Advanced Research in Material Science and Mechanical Engineering
1141-1145
页数5
DOI
出版状态已出版 - 2014
活动2013 2nd International Conference on Mechanics and Control Engineering, ICMCE 2013 - Beijing, 中国
期限: 1 9月 20132 9月 2013

出版系列

姓名Applied Mechanics and Materials
446-447
ISSN(印刷版)1660-9336
ISSN(电子版)1662-7482

会议

会议2013 2nd International Conference on Mechanics and Control Engineering, ICMCE 2013
国家/地区中国
Beijing
时期1/09/132/09/13

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