摘要
阐述了检查惯组参数稳定性传统方法的局限性以及光学捷联惯组标定参数的物理含义,然后推导了将传统标定参数转换到与惯组固联的正交坐标系的方法。对于解决检查参数稳定性时惯组各次标定参数基准不一致问题具有积极的指导意义。
In this paper, the error coefficients of strapdown inertial measurement unit （SIMU） are analyzed firstly, and the limitation of classical calibration methods is presented. Then the whole course of inductive inference is discussed in detail. This method is problem of consistent calibration standard. feasible for possessing practicability by solving the tough
出处
《航天控制》
CSCD
北大核心
2011年第2期15-16,22,共3页
Aerospace Control
