Modelling and Simulation on Multibody Dynamics for Vehicular Cold Launch Systems Based on Subsystem Synthesis Method

被引:1
|
作者
Yan Panyun [1 ]
Liang Guozhu [1 ]
Lu Yongzhi [2 ]
Qi Zhihui [2 ]
Gao Xingdou [2 ]
机构
[1] Beijing Univ Aeronaut & Astronaut, Sch Astronaut, Beijing 100191, Peoples R China
[2] Beijing Inst Space Launch Technol, Beijing 10076, Peoples R China
关键词
D O I
10.1088/1757-899X/280/1/012026
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
The fast simulation of the vehicular cold launch system (VCLS) in the launch process is an essential requirement for practical engineering applications. In particular, a general and fast simulation model of the VCLS will help the designer to obtain the optimum scheme in the initial design phase. For these purposes, a system-level fast simulation model was established for the VCLS based on the subsystem synthesis method. Moreover, a comparison of the load of a seven-axis VCLS on the rigid ground through both theoretical calculations and experiments was carried out. It was found that the error of the load of the rear left outrigger is less than 7.1%, and the error of the total load of all the outriggers is less than 2.8%. Moreover, time taken for completion of the simulation model is only 9.5 min, which is 5% of the time taken by conventional algorithms.
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页数:7
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