助推滑翔高超声速反舰导弹突防密集阵武器能力分析

摘要

在分析对比助推滑翔高超声速反舰导弹与传统反舰导弹在飞行弹道等方面差异的基础上,建立下压段导弹质心运动方程以及目标运动模型,并以满足落角约束的最优导引律作为下压段的导引律,对助推滑翔高超声速反舰导弹的飞行弹道进行仿真分析;建立密集阵武器系统与助推滑翔高超声速反舰导弹的攻防对抗仿真模型,使用蒙特卡罗法仿真计算导弹飞行速度、落地倾角等对反舰导弹突防概率的影响.通过仿真分析得出了助推滑翔高超声速反舰导弹突防密集阵武器系统的能力,为助推滑翔导弹的作战使用提供理论支撑.%On the basis of analyzing and comparing the ballistic trajectory difference between boost-glide hypersonic anti-ship missile and traditional anti-ship missile, point-mass equation for missiles and target maneuver models are built, which are founded on the optimum guidance law with a terminal angular constraint of the dive phase, simulation analysis of the bal-listic trajectory of boost-glide hypersonic anti-ship missile is conducted. Then engagement simulation models are built that be-tween boost-glide hypersonic anti-ship missile and phalanx system. The penetration probability of boost-glide hypersonic anti-ship missile is simulated by the method of Monte-Carlo, which is influenced by vehicle and path angle. The ability of boost-glide hypersonic anti-ship missile breaking the defense of phalanx system is got, which is providing theoretical support for op-erational use of boost-glide hypersonic anti-ship missile.