高、低弹道突防模型在弹道导弹仿真中的应用研究  

Research on the application of high and low trajectory penetration model for ballistic missile simulation

作　　者：麻毅威[1,2] 黄文博[1,3] 胡凡[1] 张为华 

机构地区：[1]国防科学技术大学航天科学与工程学院 [2]61541部队系统控制室 [3]北京系统工程研究所复杂系统仿真总体重点实验室

出　　处：《飞行力学》2013年第2期157-161,共5页Flight Dynamics

摘　　要：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 models are established.The comparison between standard trajectory and high/low trajectory is conducted with the numerical simulation methods,and the correctness of the high and low trajectory model is verified.Considering the high error level in the use of formula method in the process of modeling and the difficulty to determine whether they are caused by program errors during the test,the graphic method is proposed.Finally,the high and low trajectories are obtained respectively via calculation,and their characteristics are analyzed,providing reference for the selection of penetration mode.

关 键 词：高弹道 低弹道 弹道仿真 

分 类 号：TJ761.3[兵器科学与技术—武器系统与运用工程]