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建立了弹道导弹高、低弹道数学模型,并通过数值仿真分析方法将高、低弹道与标准弹道进行了对比,验证了高、低弹道数学模型的正确性。针对通常建模过程中采用公式法时存在的误差数量级过高、调试程序时难以判断是否是由程序错误导致的问题,提出了图解法,解决了这一问题。最后通过计算,得到了高、低弹道的弹道曲线,分析了其特点,为突防方式的选择提供了参考依据。
The high and low trajectory mathematical models of ballistic missiles were established. The numerical simulation analysis was used to compare the high and low trajectory with the standard trajectory. The correctness of the mathematical model of high and low trajectory was verified. In order to solve the problem, it is difficult to judge whether the errors are caused by program errors when the formula method is used. Finally, the trajectory of high and low trajectory is obtained by calculation, and its characteristics are analyzed, which provides a reference for the choice of penetration mode.