摘要
初始数学平台的确定是捷联惯导的关键,而发射前导弹的晃动给初始平台的确定带来了困难。文中首先分析了导弹的晃动规律,进而提出分别利用加速度表和陀螺仪输出的脉冲数据计算导弹的晃动角,并将其综合考虑后求取导弹平均晃动角的方法,为数学平台的建立提供了数据基础。
The calibrating of initial atti swaying missile. We analyzed the law compute the swaying angle using the swaying angle using the two kinds of rude is the key for SINS, it is very difficult to calibrate the initial attitude for a of this swaying appearance at the beginning of this paper and acquired a method to pulses data which giving by accelerometer and gyroscope, then, giving the average data.
出处
《弹箭与制导学报》
CSCD
北大核心
2007年第2期122-125,共4页
Journal of Projectiles,Rockets,Missiles and Guidance
