一种改进的捷联惯导系统姿态算法
收稿日期: 2011-08-08
网络出版日期: 2025-05-29
基金资助
总装备部重点预研项目资助
An Improved Attitude Algorithm for Strap-down Inertial Navigation System
Received date: 2011-08-08
Online published: 2025-05-29
张朝飞 , 杨孟兴 , 吴明强 . 一种改进的捷联惯导系统姿态算法[J]. 弹箭与制导学报, 2012 , 32(3) : 6 -10 . DOI: 10.15892/j.cnki.djzdxb.2012.03.012
In the attitude calculation of a strap-down inertial navigation system with rotation vector, in order to improve the accuracy of coning error compensation with certain gyro's sampling frequency, the gyro's output from current and previous updating period should be used. A general algorithm applied by N-sample used M-recurrent updating period was provided. The coefficients of this algorithm can be acquired by a simple matrix computation without deduction. Finally, this algorithm can improve the error compensation accuracy without increasing the number of sample by theory analysis and simulative results.
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