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本文提出了迎击弹道导弹的新型导弹系统方案,推导了导引方法。该导弹系统由一部可以重复使用的无人驾驶导弹发射机（MLV）和两枚反弹道导弹（ABM）组成。MLV用助推火箭发射,并根据地面或空中预警雷达及控制系统的信息计算出的飞行轨道引导至ABM的发射区。ABM为二级动力式导弹。第一级火箭用来从MLV上发射和加速ABM;第二级火箭用来修正末段弹道。由仿真证明该导弹系统与现有ABM系统相比可以扩大迎击弹道导弹的范围。
In this paper, a new missile system scheme to meet the ballistic missile is proposed, and the guidance method is derived. The missile system consists of a reusable MLV and two anti-ballistic missiles (ABMs). The MLV is guided to the launch site of the ABM by the launch of a booster rocket and flight orbit calculated from ground or airborne early warning radar and control system information. ABM is a two-stage power missile. The first stage rocket was used to launch and accelerate the ABM from the MLV; the second stage rocket was used to modify the last stage ballistic. Simulation shows that the missile system can expand the range of ballistic missiles in comparison with the existing ABM system.