摘要
研究了惯导系统空中姿态角传递对准的原理 ,推导了姿态角误差的量测方程 。
In this paper the principle of attitude transfer alignment is studied. The attitude-difference measurement equation in derived. This method is given for identification of azimuth errors in inetical platform system.
出处
《航天控制》
CSCD
北大核心
2000年第1期9-14,共6页
Aerospace Control
