摘要
介绍了综合利用地空导弹武器制导系统及弹上所提供的信息,对完全处于运动状态的导弹及目标在弹目交会阶段的数学模型进行了定量分析和计算,求解出最佳起爆延时,以及在此基础上对定向战斗部的最佳起爆方位角进行了探讨,并给出了仿真结果分析。
This paper presents a quantitative analysis and a calculation of the mathematic models of the missile in complete movement and the target in its encounter moment by using the information of the control and guide system of ground - to - air missile and the information of the missile in itself, and simultaneously finds out the optimum detonating delay time. On the basis of this, the paper also discusses the problem how to obtain the optimum detonating azimuth of directional warhead and makes an analysis of the simulation result.
出处
《空军工程大学学报(自然科学版)》
CSCD
2003年第4期19-22,共4页
Journal of Air Force Engineering University(Natural Science Edition)
关键词
定向战斗部
最佳起爆延时
最佳起爆方位角
directional warhead
optimum detonating delay time
optimum detonating azimuth