Monte Carlo ballistic simulation applied to dispersion analysis of starting control points for Antitank Missile

Yang Liu*, Kun Li, Xiaodong Song, Xiaoxian Yao

*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

This paper provides an overview of the Antitank Missile Monte Carlo starting control points dispersion analysis conducted with the ballistic simulation. First, The disturbances that affect the flight of a missile are analyzed. Then a method of how to handle with the disturbances is presented to establish a ballistic simulation model with Monte carlo method, the steps of simulating the disturbances based on Matlab are also given. Taken account of the initial angular rates disturbance, rocket engine thrust misalignment, wind disturbance, the equation that described the dynamics of the missile mass center movement should be adjusted accordingly. In this paper, a common model is established to simulate the effect of disturbances. Results indicate that missile trajectory disturbances could be substantially reduced by lowering rocket engine thrust misalignment.

源语言英语
主期刊名Proceedings of 2011 International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2011
出版商IEEE Computer Society
2929-2932
页数4
ISBN(印刷版)9781612840857
DOI
出版状态已出版 - 2011
活动2011 International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2011 - Harbin, 中国
期限: 12 8月 201114 8月 2011

出版系列

姓名Proceedings of 2011 International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2011
6

会议

会议2011 International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2011
国家/地区中国
Harbin
时期12/08/1114/08/11

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