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.
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郭振云,赵汉元.地基拦截弹对真目标进行拦截时的制导方案分析[J].国防科技大学学报,1996,18(3):40-43. Guo Zhenyun, Zhao Hanyuan. Analysis of the Guidance Scheme to Intercept the Actual Target[J]. Journal of National University of Defense Technology,1996,18(3):40-43.