Analysis for height control-loop of cruise missile to different kinds of autopilot

Qiuqiu Wen*, Qunli Xia, Chuntao Cai

*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

1 引用 (Scopus)

摘要

The models of two kinds of height control system which include the attitude autopilot inner loop and acceleration autopilot inner loop respectively are built. The response rate, stabilization and engineer realization of gravity compensation of the height control systems are analyzed and compared. The result shows that they have same performances and can be used both in missile altitude control. The gravity compensation can improve the transition quality of height control and decrease the overshoot. The gravity compensation command matching attitude autopilot depends on the flying parameter heavily, so the engineer reliability is lower than acceleration autopilot.

源语言英语
主期刊名Advances in Automation and Robotics, Vol. 2 - Selected Papers from the 2011 International Conference on Automation and Robotics, ICAR 2011
507-514
页数8
DOI
出版状态已出版 - 2011
活动2011 International Conference on Automation and Robotics, ICAR 2011 - Dubai, 阿拉伯联合酋长国
期限: 1 12月 20112 12月 2011

出版系列

姓名Lecture Notes in Electrical Engineering
123 LNEE
ISSN(印刷版)1876-1100
ISSN(电子版)1876-1119

会议

会议2011 International Conference on Automation and Robotics, ICAR 2011
国家/地区阿拉伯联合酋长国
Dubai
时期1/12/112/12/11

指纹

探究 'Analysis for height control-loop of cruise missile to different kinds of autopilot' 的科研主题。它们共同构成独一无二的指纹。

引用此