Low-end MEMS IMU can contribute in GPS/INS deep integration

Yalong Ban, X. Niu, Tisheng Zhang, Quan Zhang, Wenfei Guo, Hongping Zhang
{"title":"Low-end MEMS IMU can contribute in GPS/INS deep integration","authors":"Yalong Ban, X. Niu, Tisheng Zhang, Quan Zhang, Wenfei Guo, Hongping Zhang","doi":"10.1109/PLANS.2014.6851440","DOIUrl":null,"url":null,"abstract":"In a deeply-coupled GPS/INS integrated system, the use of the inertial aiding information can improve the tracking loop performance and make the system more robust. To meet this requirement, the inertial aiding information should have sufficient accuracy in short-term (such as the sampling interval of GPS, e.g. 1sec). The MEMS (Micro-Electro Mechanical System) IMU (Inertial Measurement Unit) can be a promising candidate due to its small size and low cost. There should be no doubt that MEMS INS (Inertial Navigation System) can aid the GPS receiver tracking loop by eliminating the dominant part of the motion dynamic stress, considering that the INS errors induced by the receiver motion dynamics is much less than the motion dynamic itself, when the receiver manoeuvres. So the only concern the side effect caused by MEMS INS, which determine whether MEMS IMU is qualified for deep integration, is its navigation error independent with the motion dynamics (i.e. manoeuvre-independent error). This paper assesses this side effect of MEMS INS in terms of providing Doppler aiding data in to the GPS carrier tracking loop through a thorough error propagation analysis. The Laplace transform analysis is applied to the simplified INS error dynamic equations under stationary condition and find out the transfer relation between the error sources and the velocity estimation errors. Then the velocity error is converted to Doppler aiding error and substitute into the GPS tracking loop to analyze the corresponding carrier phase error. Results show that the largest velocity error caused by maneuver-independent errors is less than 0.1m/s during the typical GPS update interval (e.g. 1 sec), which meets the real road test results. The consequent carrier phase tracking error caused by the maneuver-independent error of MEMS INS is below 1.2 degree, which is much less than receiver inherent errors (e.g. the oscillator error and thermal noise). Conclusion can be reached that even the low-end MEMS IMUs have the ability of aiding the GPS receiver signal tracking although it induces some additional errors.","PeriodicalId":371808,"journal":{"name":"2014 IEEE/ION Position, Location and Navigation Symposium - PLANS 2014","volume":"7 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2014-05-05","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"18","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"2014 IEEE/ION Position, Location and Navigation Symposium - PLANS 2014","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/PLANS.2014.6851440","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 18

Abstract

In a deeply-coupled GPS/INS integrated system, the use of the inertial aiding information can improve the tracking loop performance and make the system more robust. To meet this requirement, the inertial aiding information should have sufficient accuracy in short-term (such as the sampling interval of GPS, e.g. 1sec). The MEMS (Micro-Electro Mechanical System) IMU (Inertial Measurement Unit) can be a promising candidate due to its small size and low cost. There should be no doubt that MEMS INS (Inertial Navigation System) can aid the GPS receiver tracking loop by eliminating the dominant part of the motion dynamic stress, considering that the INS errors induced by the receiver motion dynamics is much less than the motion dynamic itself, when the receiver manoeuvres. So the only concern the side effect caused by MEMS INS, which determine whether MEMS IMU is qualified for deep integration, is its navigation error independent with the motion dynamics (i.e. manoeuvre-independent error). This paper assesses this side effect of MEMS INS in terms of providing Doppler aiding data in to the GPS carrier tracking loop through a thorough error propagation analysis. The Laplace transform analysis is applied to the simplified INS error dynamic equations under stationary condition and find out the transfer relation between the error sources and the velocity estimation errors. Then the velocity error is converted to Doppler aiding error and substitute into the GPS tracking loop to analyze the corresponding carrier phase error. Results show that the largest velocity error caused by maneuver-independent errors is less than 0.1m/s during the typical GPS update interval (e.g. 1 sec), which meets the real road test results. The consequent carrier phase tracking error caused by the maneuver-independent error of MEMS INS is below 1.2 degree, which is much less than receiver inherent errors (e.g. the oscillator error and thermal noise). Conclusion can be reached that even the low-end MEMS IMUs have the ability of aiding the GPS receiver signal tracking although it induces some additional errors.
低端MEMS IMU有助于GPS/INS的深度集成
在GPS/INS深度耦合集成系统中,利用惯性辅助信息可以提高跟踪回路的性能,增强系统的鲁棒性。为了满足这一要求,惯性辅助信息在短期内(如GPS的采样间隔,如1秒)应具有足够的精度。MEMS(微机电系统)惯性测量单元(IMU)因其体积小、成本低而成为一个有前途的候选器件。考虑到接收机运动时由接收机运动动力学引起的惯性导航系统误差远小于运动动力学本身,因此MEMS INS (Inertial Navigation System)可以通过消除运动动态应力的主导部分来辅助GPS接收机跟踪环路,这一点毋庸置疑。因此,决定MEMS IMU是否具有深度集成资格的唯一关注的副作用是其与运动动力学无关的导航误差(即与机动无关的误差)。本文通过全面的误差传播分析,评估了MEMS INS在向GPS载波跟踪环路提供多普勒辅助数据方面的这种副作用。对平稳条件下简化的惯导系统误差动力学方程进行拉普拉斯变换分析,找出误差源与速度估计误差之间的传递关系。然后将速度误差转化为多普勒辅助误差,代入GPS跟踪环路,分析相应的载波相位误差。结果表明,在典型的GPS更新间隔(如1秒)内,机动无关误差导致的最大速度误差小于0.1m/s,符合实际路测结果。由机动无关误差引起的载波相位跟踪误差小于1.2度,远小于接收机固有误差(如振荡器误差和热噪声)。可以得出结论,即使是低端的MEMS imu也具有辅助GPS接收机信号跟踪的能力,尽管它会产生一些额外的误差。
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 求助全文
来源期刊
自引率
0.00%
发文量
0
×
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
确定
请完成安全验证×
copy
已复制链接
快去分享给好友吧!
我知道了
右上角分享
点击右上角分享
0
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 布克学术 All rights reserved.
京ICP备2023020795号-1
ghs 京公网安备 11010802042870号
Book学术文献互助
Book学术文献互助群
群 号:481959085
Book学术官方微信