首页 | 本学科首页   官方微博 | 高级检索  
     

一种提高捷联惯导系统静态初始对准精度的方法
引用本文:何洪文,胡昌华,黄海,袁静.一种提高捷联惯导系统静态初始对准精度的方法[J].电光与控制,2005,12(5):58-61.
作者姓名:何洪文  胡昌华  黄海  袁静
作者单位:西安第二炮兵工程学院,陕西,西安,710025
摘    要:针对目前提高捷联惯导系统自对准精度难度大这一情况,在建立SINS静基座初始对准的误差方程的基础上,通过对影响对准精度的误差因素进行分析,提出了一种在载体内部安装高精度自主寻北装置的方法,该方法可有效地提高初始对准精度。

关 键 词:捷联惯导系统  自对准  陀螺仪  捷联矩阵
文章编号:1671-637X(2005)05-0058-04
收稿时间:2004-10-01
修稿时间:2004-10-012004-10-18

A method for improving the static-state initial alignment accuracy of SINS
HE Hong-wen,Hu Chang-hua,HUANG Hai,YUAN Jing.A method for improving the static-state initial alignment accuracy of SINS[J].Electronics Optics & Control,2005,12(5):58-61.
Authors:HE Hong-wen  Hu Chang-hua  HUANG Hai  YUAN Jing
Abstract:Based on the fact that it is very difficult to improve the autonomous alignment accuracy of strapdown inertial navigation system(SINS),an error function for static-state initial alignment of SINS is built.Then an analysis is made for the factors which have effect on the alignment accuracy,and a method is put forward for installing a high-accuracy,auto-north-seeker in the carrier,which can improve the alignment accuracy effectively.
Keywords:strapdown inertial navigation system(SINS)  autonomous alignment  gyroscope  strapdown matrix
本文献已被 CNKI 维普 万方数据 等数据库收录!
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号