摘要
基于模态综合法方法,利用ADAMS和ANSYS建立了导弹发射系统的刚柔耦合模型,通过对发射过程动力学仿真分析,获得了导弹的发射姿态和发射系统的动力学特性,分析结果通过试验进行了验证。
Based on the method of component model synthesis, a rigid-flexible coupling model of missile launcher is built by the ADAMS and ANSYS. The dynamic characteristics of missile attitude and launching system have been obtained through the dynamic analysis of the launching process. Its results have been proved by tests
出处
《导弹与航天运载技术》
北大核心
2009年第6期51-54,共4页
Missiles and Space Vehicles
关键词
倾斜发射
发射车
发射动力学
刚柔耦合
Oblique launching
Missile launcher
Dynamic analysis of launching
Rigid-flexible coupling
