Analysis of a Missile's Initial Disturbance

Abstract:

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 .

• Periodical: Advanced Materials Research (Volumes 889-890)
• Pages: 152-155
• DOI: https://doi.org/10.4028/www.scientific.net/AMR.889-890.152
• Online since: February 2014
• Authors: Xin Lin Wei, Yi Jiang
• Keywords: ABAQUS, Dynamic Analysis, Vehicle Missile

References

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