TY - GEN
T1 - Analysis of a missile's initial disturbance
AU - Wei, Xin Lin
AU - Jiang, Yi
PY - 2014
Y1 - 2014
N2 - 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.
AB - 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.
KW - ABAQUS
KW - Dynamics analysis
KW - Vehicle missile
UR - http://www.scopus.com/inward/record.url?scp=84896833259&partnerID=8YFLogxK
U2 - 10.4028/www.scientific.net/AMR.889-890.152
DO - 10.4028/www.scientific.net/AMR.889-890.152
M3 - Conference contribution
AN - SCOPUS:84896833259
SN - 9783038350156
T3 - Advanced Materials Research
SP - 152
EP - 155
BT - Engineering Solutions for Manufacturing Processes IV
T2 - 2013 4th International Conference on Advances in Materials and Manufacturing, ICAMMP 2013
Y2 - 18 December 2013 through 19 December 2013
ER -