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高精度捷联惯导系统的系统级标定方法

康宇航 周绍磊 匡宇 祁亚辉

兵工自动化Issue(10):53-57,5.
兵工自动化Issue(10):53-57,5.DOI:10.7690/bgzdh.2013.10.015

高精度捷联惯导系统的系统级标定方法

Systematic Calibration Method for High-Precision Strapdown Inertial Navigation System

康宇航 1周绍磊 1匡宇 2祁亚辉1

作者信息

  • 1. 海军航空工程学院控制科学与工程系,山东 烟台 264000
  • 2. 江西农业大学计算机与信息工程学院,南昌 330045
  • 折叠

摘要

Abstract

Aiming at the large error of current calibration method, and error is increased when position departure increasing, put forward a iterative solution method. Based on the general output model of the high-precision strapdown inertial navigation system (SINS), the error model of the output can be derived. Then through proper positions and rotations, exciting speed error of the navigation systems, the error parameters can be deduced. Then with iterative algorithm, model parameters can be corrected continuously and navigation error would decrease as well. The analysis results prove that the method is very simple, has high calibration precision and without strictly level and north seeking. It meets requirements of navigation with high practical value in engineering.

关键词

捷联惯导系统/系统级标定/最小二乘/迭代

Key words

strapdown inertial navigation system(SINS)/systematic calibration/least square/iterative

分类

军事科技

引用本文复制引用

康宇航,周绍磊,匡宇,祁亚辉..高精度捷联惯导系统的系统级标定方法[J].兵工自动化,2013,(10):53-57,5.

基金项目

国家自然科学基金资助项目(61203168) (61203168)

兵工自动化

OACSTPCD

1006-1576

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