基于ADAMS的导轨式导弹发射装置发射姿态研究

摘要

A multi-rigid body model of dynamic simulation was established by virtual prototype technology.The displacement of missile three slider trend verified the changes of missile pitch angle,and the change trend of missile attitude was analyzed by launching system during launching,and comparing the influence of the missile attitude by launching by comparing the variety of rail parameter,we provided the basis for the design of the guide rails.%采用虚拟样机方法,建立了导弹发射装置导弹发射时脱离轨道姿态的多体动力学模型,通过导弹3个滑块的位移变化趋势和导弹俯仰角的变化,分析了导弹在发射过程中的姿态变化趋势和对导弹发射姿态影响的导引面参数,为导弹发射装置导轨导引面的设计提供依据.