敏捷导弹的末制导系统性能综合分析  

Comprehensive Analysis of Terminal Guidance System for Agile Missile

作　　者：季登高[1] 黄兴李[1] 郭振西[1] 

机构地区：[1]北京临近空间飞行器系统工程研究所,北京100076

出　　处：《弹箭与制导学报》2012年第4期80-83,88,共5页Journal of Projectiles,Rockets,Missiles and Guidance

摘　　要：分析末制导系统的有限时间稳定性以及末制导的需用过载,建立末制导回路动态品质与系统性能之间的关系,并讨论直接力的引入时机问题,最后对敏捷导弹的末制导精度进行分析,得到脱靶量、飞行控制系统性能、探测系统性能、量测噪声以及目标机动的关系,结果表明敏捷导弹对探测系统的性能提出了更高的要求。The finite-time stability and required overload in terminal guidance phase analyzed. The relation between terminal guidance dy- namics and system performance established. Based on this, the occasion of introduction for the direct force discussed. By analyzing the ter- minal guidance precision, the relations miss distance, control system performance, detective system performz：nce, measure noise and target maneuver shown up. The results show that agile missile has higher requirements on the detective system performance.

关 键 词：末制导 敏捷导弹 性能分析 有限时间 脱靶量 需用过载 

分 类 号：TJ765.3[兵器科学与技术—武器系统与运用工程]