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给出一种可模拟假弹头的整流罩结构,应用分析力学Lagrange方程对假弹头变形过程进行了动力学分析,最后通过算例验证了结构的可行性,分析了影响假弹头飞行轨迹的主要因素,得出飞行轨迹变化与弹簧倔强系数和最大压缩量有关的结论。
A kind of fairing structure which can simulate the warhead is given. The kinematics analysis of the warhead deformation process is carried out by Lagrange equation. Finally, an example is given to verify the feasibility of the structure. The main factors affecting the flight path of the warhead are analyzed. , Draw the conclusion that the change of flight path is related to the coefficient of stubbornness and the maximum compression.