Firstly, the diagram of the mechanism and the kinematics model is established. Afterward, on the basis of this, the kinematics simulation of the missile ejection mechanism is accomplished.
首先建立了该系统的物理模型和结构简图，在分析机构的运动过程的基础上，建立了运动学模型，并对导弹弹射机构的运动学模型进行了仿真。
参考来源 - 飞机导弹弹射系统动特性分析和仿真研究·2,447,543篇论文数据，部分数据来源于NoteExpress
弹射机构的应用场合对系统的重量、动态响应性有严格要求，对控制元件的动态响应和重量要求也很苛刻。
The application of ejection mechanism usually has a strict demand on its weight and performance, even much stricter on the dynamic response of its control components.
设计了一种同步机构，应用于某垂直弹射装置中以满足其弹射要求。
A synchronization mechanism was designed to satisfy ejection requirements of vertical ejection equipment.
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