摘要
主要研究了其在动基座条件下的误差方程,进行了误差方程的分析,并用广义卡尔曼滤波方法进行了动基座条件下MEMS惯性测量组件的对准研究。最后,给出了该对准方法的仿真结果。
The paper mainly research on the error equation of its in-motion, and analysing them. Except of these,the paper also studies the alignment of its in-motin in the way of extend Kalman filter. The simulation result of the alignment method is provided in the end of the paper.
出处
《弹箭与制导学报》
CSCD
北大核心
2007年第5期59-60,64,共3页
Journal of Projectiles,Rockets,Missiles and Guidance