Navigation Error Analysis in Strapdown Inertial Navigation

A. Shkel, Yusheng Wang
{"title":"Navigation Error Analysis in Strapdown Inertial Navigation","authors":"A. Shkel, Yusheng Wang","doi":"10.1002/9781119699910.ch4","DOIUrl":null,"url":null,"abstract":"One of the most important characteristics of an inertial navigation system is its navigation accuracy, which is directly related to the measurement errors of the inertial measurement unit (IMU). This chapter analyses the relation between the IMU error and the navigation error in the strapdown inertial navigation. It introduces the terminology, origin, and characteristics of some of the major error sources. Error sources in navigation can be categorized into three groups: IMU errors, initial calibration errors, and numerical errors. Assembly errors mainly come from the shift of the mounting direction of individual inertial sensors from their ideal orientations. The position error will exceed a meter of error within a few seconds of navigation with unaided consumer grade IMUs. Tactical grade IMUs have the capability of attitude measurement with reasonable errors and are able to conduct short‐term navigation, with navigation accuracy on the order of meters within 30 seconds of strapdown inertial navigation.","PeriodicalId":371531,"journal":{"name":"Pedestrian Inertial Navigation with Self‐Contained Aiding","volume":"82 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1900-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Pedestrian Inertial Navigation with Self‐Contained Aiding","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1002/9781119699910.ch4","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 0

Abstract

One of the most important characteristics of an inertial navigation system is its navigation accuracy, which is directly related to the measurement errors of the inertial measurement unit (IMU). This chapter analyses the relation between the IMU error and the navigation error in the strapdown inertial navigation. It introduces the terminology, origin, and characteristics of some of the major error sources. Error sources in navigation can be categorized into three groups: IMU errors, initial calibration errors, and numerical errors. Assembly errors mainly come from the shift of the mounting direction of individual inertial sensors from their ideal orientations. The position error will exceed a meter of error within a few seconds of navigation with unaided consumer grade IMUs. Tactical grade IMUs have the capability of attitude measurement with reasonable errors and are able to conduct short‐term navigation, with navigation accuracy on the order of meters within 30 seconds of strapdown inertial navigation.
查看原文
分享 分享
微信好友 朋友圈 QQ好友 复制链接
本刊更多论文
捷联惯性导航中的导航误差分析
惯性导航系统最重要的特性之一是导航精度,而导航精度直接关系到惯性测量单元的测量误差。本章分析了捷联惯性导航中IMU误差与导航误差之间的关系。它介绍了一些主要误差源的术语、来源和特征。导航中的误差源可分为三大类:IMU误差、初始标定误差和数值误差。装配误差主要来自于单个惯性传感器的安装方向偏离其理想方向。使用独立的消费级imu,定位误差将在几秒钟内超过一米。战术级imu具有合理误差的姿态测量能力,能够进行短期导航,在捷联惯性导航30秒内的导航精度在米数量级。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
求助全文
约1分钟内获得全文 去求助
来源期刊
自引率
0.00%
发文量
0
期刊最新文献
Perspective on Pedestrian Inertial Navigation Systems Sensor Fusion Approaches Zero‐Velocity Update Aided Pedestrian Inertial Navigation Index Adaptive ZUPT‐Aided Pedestrian Inertial Navigation
×
引用
GB/T 7714-2015
复制
MLA
复制
APA
复制
导出至
BibTeX EndNote RefMan NoteFirst NoteExpress
×
×
提示
您的信息不完整,为了账户安全,请先补充。
现在去补充
×
提示
您因"违规操作"
具体请查看互助需知
我知道了
×
提示
现在去查看 取消
×
提示
确定
0
微信
客服QQ
Book学术公众号 扫码关注我们
反馈
×
意见反馈
请填写您的意见或建议
请填写您的手机或邮箱
已复制链接
已复制链接
快去分享给好友吧!
我知道了
×
扫码分享
扫码分享
Book学术官方微信
Book学术文献互助
Book学术文献互助群
群 号:481959085
Book学术
文献互助 智能选刊 最新文献 互助须知 联系我们:info@booksci.cn
Book学术提供免费学术资源搜索服务,方便国内外学者检索中英文文献。致力于提供最便捷和优质的服务体验。
Copyright © 2023 Book学术 All rights reserved.
ghs 京公网安备 11010802042870号 京ICP备2023020795号-1