多管火箭发射动力学普遍方程的研究

多管火箭武器系统的总体论证，总体设计，需要对系统进行发射动力学分析。该文用图论的观点分析多管火箭发射系统的结构，用多刚体动力学的分析方法，把多管火箭系统风化为火箭弹，俯仰部分，回转部分和载体部分４部分刚体，适当改进了多刚体动力学中动力学增广体的概念，使之更适合于多管火箭武器这一特殊系统的发射动力学分析。

The Study of Generalized Dynamical Equations for Launching System of Multiple Launch Rocket

The overall demonstration and overall design of the multiple launching rocket system, is needed to make. In this paper,the structure of the multiple launching rocket system is analized from the viewpoint of graph theory,and by the analitical method of multi rigid body dynamics,the multiple launching rocket system is rigidized into four rigid parts, including rocket,piching part,rotary part and carrier.The proper improvement of the dynamical augment body concept of multi rigid body dynamics makes it more suitable to launching dynamics analysis of multiple launching rocket system.In the end,the generalized launching dynamics equations of matrix form with tensor and vector for multiple launching rocket system is set up.It makes it convenienk to make launching dynamics analysis.