An intelligent parameter space approach applicable to engineering design of missile autopilot

Jing Mei Lou, Ke Zhang

科研成果: 书/报告/会议事项章节会议稿件同行评审

2 引用 (Scopus)

摘要

Intelligent control is one of the development directions of control theory. The parameter space approach is used to solve robust stability problem of the system with uncertain parameters. This paper presents an intelligent parameter space approach that applied to design the missile autopilot. The method combines parameter space approach with intelligent PID. In order to research and prove the approach by computer simulation, multi-mode models are set channel control augmentation loop of missile. The conclusion is that this approach can improve control quality.

源语言英语
主期刊名Proceedings - 2009 International Conference on Information Engineering and Computer Science, ICIECS 2009
DOI
出版状态已出版 - 2009
活动2009 International Conference on Information Engineering and Computer Science, ICIECS 2009 - Wuhan, 中国
期限: 19 12月 200920 12月 2009

出版系列

姓名Proceedings - 2009 International Conference on Information Engineering and Computer Science, ICIECS 2009

会议

会议2009 International Conference on Information Engineering and Computer Science, ICIECS 2009
国家/地区中国
Wuhan
时期19/12/0920/12/09

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