固体火箭技术2011，Vol.34Issue(5)：559-563,5.
基于改进Craig-Bampton法的导弹发射过程多柔体动力学研究
Flexible multi-body dynamics analysis during missile launching based on improved Craig-Bampton method
摘要
Abstract
The rigid-flexible coupling system dynamics method was applied,the key parts and components such as the frame and undercarriage were regarded as the flexible bodies and were merged into the multi-body dynamics model of vehicular missile launching system with improved Craig-Bampton method. The dynamic model of flexible multibody systems was established and simulation was performed during launching. The dynamic characteristics of missile attitude parameter and launching system were obtained , and the results were compared with that of the rigid model. The results show that rigid-flexible multi-body coupling model is very close to actual launch situation of missile. It provides a theoretical foundation for investigating dynamic characteristics and analysing the initial disturbance accurately during the launching process of a vehicular missile.关键词
车载导弹/柔性多体动力学/发射过程/改进的Craig-Bampton法:姿态Key words
vehicular missile launcher/flexible multi-body dynamics/launching process/improved Craig-Bampton method attitude分类
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高星斗,毕世华,陈阵..基于改进Craig-Bampton法的导弹发射过程多柔体动力学研究[J].固体火箭技术,2011,34(5):559-563,5.基金项目
总装备部重点预研项目(10403010302). （10403010302）
