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基于卡尔曼滤波技术解算惯导的水平偏差
引用本文:郭立红,朱玮,李岩,李艳平. 基于卡尔曼滤波技术解算惯导的水平偏差[J]. 光学精密工程, 2003, 11(4): 379-383
作者姓名:郭立红  朱玮  李岩  李艳平
作者单位:中国科学院,长春光学精密机械与物理研究所,吉林,长春,130022
摘    要:针对测量船惯导系统水平及航向精度检测需求,提出了采用卡尔曼滤波技术解算惯导水平偏差的新方法。对经纬仪校准惯导的基本原理及陀螺的随机飘移分析,利用经纬仪测星方法,在惯导飘移误差小于7′,标定误差可在2″以内,可有效地消除惯导的随机游动误差分量,将使测量船的整体测量精度得到显著的提高。

关 键 词:惯性导航系统  卡尔曼滤波  校准
文章编号:1004-924X(2003)04-0379-05
收稿时间:2003-01-16
修稿时间:2003-01-16

Using Kalmen filter technology establishment of attitude and course errors for measurement ship inertial navigation system
GUO Li-hong,ZHU Wei,LI Yan,LI Yan-ping . Using Kalmen filter technology establishment of attitude and course errors for measurement ship inertial navigation system[J]. Optics and Precision Engineering, 2003, 11(4): 379-383
Authors:GUO Li-hong  ZHU Wei  LI Yan  LI Yan-ping 
Affiliation:Changchun Institute of Optics, Fine Mechanics and Physics, Chinese Academy of Sciecces, Changchun 130022, China
Abstract:In order to satisfy the need of testing the attitude and course of INS of measurement ship, the paper proposes a new method of using the Kalmen Filter to work out the attitude and course error. Analyzing the fundamental of INS calibration by theodolite and random wave of top. The calibrating attitude and course error of INS would deduce random wave error, so as to increase the measuring precision of the ship.
Keywords:INS  Kalmen filter  calibration
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