摘要
捷联惯导系统初始对准中利用卡尔曼滤波器进行状态估计时,其数学平台的东向和北向水平失准角估计速度很快,而天向方位失准角的收敛很慢。为了解决这个问题,在基本卡尔曼滤波的基础上引入了多级组合滤波的思想,利用对捷联矩阵的修正和对天向方位失准角φU估计的改进产生了新的信息,形成了两级卡尔曼滤波,并且与小波软阈值法相结合,实现了捷联惯导系统的快速初始对准。
In SINS initial alignment, east and north level error angles can be perfectly acquired by Kalman filtering, whereas the estimation effect of azimuth error angle φU was bad. The multi-stage integrated filtering was proposed. The new information of attitude matrix and the new estimation method of azimuth error angle φU was used by the new filtering, also the de-nosing by soft thresholding methods was utilized to eliminate the noise. The simulation shows that the time of initial alignment reduces greatly, the new fast estimation method performs better.
出处
《系统仿真学报》
EI
CAS
CSCD
北大核心
2008年第23期6377-6379,共3页
Journal of System Simulation
基金
国家部委(总装)预研项目(51405030104BQ0171)