Analysis of a missile's initial disturbance

Xin Lin Wei, Yi Jiang

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

In this paper, a certain type of vehicle missile launching system is the research object, which uses CAE technology to make a flexible coupling system dynamics simulation and analysis to provide a reference for similar tests. Since the complex structure of the vehicle missile system, reasonable assumptions and simplifications are made in establishing the dynamics model. Pro/E is used to build the three-dimensional model, and then it is imported to the ABAQUS to establish its dynamics model. Finally, in a complete virtual prototyping system model, we make a simulation of working conditions, and draw conclusions and analysis. The results show that the use of independent dynamics rigid-flexible coupling model dynamics simulation based on ABAQUS can be more realistic simulation of the process of vehicle missile launch, and it verifies the results of different working conditions, which provides a reference for the vehicle missile launching systems simulation.

源语言英语
主期刊名Engineering Solutions for Manufacturing Processes IV
152-155
页数4
DOI
出版状态已出版 - 2014
活动2013 4th International Conference on Advances in Materials and Manufacturing, ICAMMP 2013 - Kunming, 中国
期限: 18 12月 201319 12月 2013

出版系列

姓名Advanced Materials Research
889-890
ISSN(印刷版)1022-6680

会议

会议2013 4th International Conference on Advances in Materials and Manufacturing, ICAMMP 2013
国家/地区中国
Kunming
时期18/12/1319/12/13

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