助推滑翔高超声速反舰导弹多方向协同突防可行性研究

摘要

On the basis of analyzing the ballistic trajectory character of boost-glide hypersonic anti-ship missile,some possible penetration strategy is designed.Point-mass equation for missiles is built,and the feasibility of muti-directional penetration of multi-missiles in coordination which launching by single platform is studied,which is based on the optimum guidance law with a terminal angular constraint.Some conclusions are obtained through simulation that the muti-directional penetration of multi-missiles in coordination which launching by single platform is feasible by manually setting virtual targets under the constraints,such as the normal overload,trajectory inclination angle,dynamic pressure.%在分析助推滑翔高超声速反舰导弹弹道特点的基础上,设计可能的多弹协同突防策略;建立下压段导弹质心运动方程,并在满足落角约束的最优导引律条件下,分析单平台发射多枚导弹多方向协同突防的可行性.通过仿真得出助推滑翔高超声速反舰导弹在过载、落地倾角、动压等条件的约束下,采用人工设置虚拟目标的方式进行单平台多弹多方向协同突防具有可行性.