摘要
从新一代空空导弹的发展对惯性制导技术的需求出发 ,论述了惯导系统的功能、总体精度分析设计、惯性元件选型、初始对准及机载数据链系统设计上存在的几个问题 。
From the viewpoint of the IGS development of air to air missiles, some design problems, such as the function of IGS, system accuracy analysis, design of inertial untis, initial alignment techniqes and airbone data link systems, are studied. Some methods to solve these problems in engineering practice are given.
出处
《制导与引信》
2003年第1期1-5,共5页
Guidance & Fuze
关键词
惯性制导系统
设计
初始对准
空对空导弹
air to air missile
inertial guidance
accuracy analysis
initial alignment
data link
