助推滑翔高超声速反舰导弹末制导雷达搜索过程分析

摘要

在分析助推滑翔高超声速反舰导弹飞行弹道特点的基础上,建立了末制导雷达搜索过程仿真模型,并使用蒙特卡罗法仿真计算了在自控终点散布误差、导弹飞行速度、目标散布等因素影响下的末制导雷达搜索面积及捕捉概率.通过仿真分析得出了助推滑翔高超声速反舰导弹末制导雷达的搜索规律,为助推滑翔导弹的作战使用提供理论支撑.%On the basis of analyzing the ballistic trajectory character of boost-glide hypersonic anti-ship missile, the process of terminal guidance radar searching target is described. The detectable area and acquisiton probability are simulated by the method of Monte-Carlo,which are influenced by autocontrol end-poingt scattering accuracy,missile velocity,target`s diffuxing and so on. The law of terminal guidance radar searching is got,which is providing theoretical support for operational use of boost-glide hypersonic anti-ship missile.