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

作　　者：郭振云[1] 赵汉元[1] 

机构地区：[1]国防科技大学自动控制系

出　　处：《国防科技大学学报》1996年第3期40-43,共4页Journal of National University of Defense Technology

摘　　要：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.

关 键 词：制导 拦截 目标 导弹 地基拦截弹 

分 类 号：TJ765.3[兵器科学与技术—武器系统与运用工程]