Design and analysis of missile two-loop autopilot with PI compensator under multi-constraints

Hui Wang*, De Fu Lin, Jiang Wang, Zhen Xuan Cheng

*此作品的通讯作者

科研成果: 书/报告/会议事项章节会议稿件同行评审

4 引用 (Scopus)

摘要

In order to eliminate the static error, PI compensator was introduced to the classic two-loop autopilot and the contribution of PI was analyzed while the equivalent time constant estimates of two-loop autopilot with PI was discussed. Four different objective functions were introduced to the design procedures. It is concluded that it is the large gain at low frequency of PI solved the problem of static error.

源语言英语
主期刊名ICACTE 2010 - 2010 3rd International Conference on Advanced Computer Theory and Engineering, Proceedings
V5117-V5121
DOI
出版状态已出版 - 2010
活动2010 3rd International Conference on Advanced Computer Theory and Engineering, ICACTE 2010 - Chengdu, 中国
期限: 20 8月 201022 8月 2010

出版系列

姓名ICACTE 2010 - 2010 3rd International Conference on Advanced Computer Theory and Engineering, Proceedings
5

会议

会议2010 3rd International Conference on Advanced Computer Theory and Engineering, ICACTE 2010
国家/地区中国
Chengdu
时期20/08/1022/08/10

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