地基拦截弹对真目标进行拦截时的制导方案分析

Analysis of the Guidance Scheme to Intercept the Actual Target

讨论了地基拦截弹对真目标（中近程弹道式导弹）进行拦截时的制导方案。根据拦截弹的飞行特点，将拦截过程分为初始段、中间段和拦截段，并采取了相应的制导方案。仿真结果表明，拦截具有较高的精度和良好的弹道特性，此方案是可行的。

This paper studies the guidance scheme of the interception missile to intercept the actual target which is an intermediate or short range ballistic missile. According to the interception missile's flight characteristics, the trajectory is divided into three phases: primary,middle and interception phase, with variant guidance schemes. The simulation has proved that the schemes are feasible and the result is satisfactory.