惯性仪表误差补偿技术在提高战略导弹精度中的应用  

Application of Error compensation Technology of Inertial Instruments in Improvement of Strategic Ballistic Missile Accuracy

作　　者：朱振乾[1] 

机构地区：[1]北京航天自动控制研究所

出　　处：《航天控制》1995年第3期1-9,共9页Aerospace Control

摘　　要：本文对有关战略导弹惯性仪表主要误差源的分类及对精度的影响；惯性仪表误差补偿的各种方法及其优缺点等内容作了介绍，对美国洲际导弹误差补偿方法也作了介绍，最后对惯性仪表误差的几种补偿方案作了分析。In this paper,classification of the inertial instrument primary error sources of strategic missile and their influences on accuracy,as well as various methods of error compensation and advantages or shortages of them are presented.Methods used in U.S.A for intercontinental ballistic missille are also introduced.Finally,several inertial instrument error compensation shemes are analyzed.

关 键 词：制导精度 误差补偿 战略导弹 惯性仪表 

分 类 号：TJ765[兵器科学与技术—武器系统与运用工程]