• 文献检索
  • 文档翻译
  • 深度研究
  • 学术资讯
  • Suppr Zotero 插件Zotero 插件
  • 邀请有礼
  • 套餐&价格
  • 历史记录
应用&插件
Suppr Zotero 插件Zotero 插件浏览器插件Mac 客户端Windows 客户端微信小程序
定价
高级版会员购买积分包购买API积分包
服务
文献检索文档翻译深度研究API 文档MCP 服务
关于我们
关于 Suppr公司介绍联系我们用户协议隐私条款
关注我们

Suppr 超能文献

核心技术专利:CN118964589B侵权必究
粤ICP备2023148730 号-1Suppr @ 2026

文献检索

告别复杂PubMed语法,用中文像聊天一样搜索,搜遍4000万医学文献。AI智能推荐,让科研检索更轻松。

立即免费搜索

文件翻译

保留排版,准确专业,支持PDF/Word/PPT等文件格式,支持 12+语言互译。

免费翻译文档

深度研究

AI帮你快速写综述,25分钟生成高质量综述,智能提取关键信息,辅助科研写作。

立即免费体验

一种用于低成本陆地车辆GPS/MEMS-INS姿态确定的性能改进方法。

A performance improvement method for low-cost land vehicle GPS/MEMS-INS attitude determination.

作者信息

Cong Li, Li Ercui, Qin Honglei, Ling Keck Voon, Xue Rui

机构信息

School of Electronic and Information Engineering, Beihang University, 37 Xueyuan Road, Haidian District, Beijing 100191, China.

School of Electrical and Electronic Engineering, Nanyang Technological University, 50 Nangyang Avenue 639798, Singapore.

出版信息

Sensors (Basel). 2015 Mar 9;15(3):5722-46. doi: 10.3390/s150305722.

DOI:10.3390/s150305722
PMID:25760057
原文链接:https://pmc.ncbi.nlm.nih.gov/articles/PMC4435141/
Abstract

Global positioning system (GPS) technology is well suited for attitude determination. However, in land vehicle application, low-cost single frequency GPS receivers which have low measurement quality are often used, and external factors such as multipath and low satellite visibility in the densely built-up urban environment further degrade the quality of the GPS measurements. Due to the low-quality receivers used and the challenging urban environment, the success rate of the single epoch ambiguity resolution for dynamic attitude determination is usually quite low. In this paper, a micro-electro-mechanical system (MEMS)-inertial navigation system (INS)-aided ambiguity resolution method is proposed to improve the GPS attitude determination performance, which is particularly suitable for land vehicle attitude determination. First, the INS calculated baseline vector is augmented with the GPS carrier phase and code measurements. This improves the ambiguity dilution of precision (ADOP), resulting in better quality of the unconstrained float solution. Second, the undesirable float solutions caused by large measurement errors are further filtered and replaced using the INS-aided ambiguity function method (AFM). The fixed solutions are then obtained by the constrained least squares ambiguity decorrelation (CLAMBDA) algorithm. Finally, the GPS/MEMS-INS integration is realized by the use of a Kalman filter. Theoretical analysis of the ADOP is given and experimental results demonstrate that our proposed method can significantly improve the quality of the float ambiguity solution, leading to high success rate and better accuracy of attitude determination.

摘要

全球定位系统(GPS)技术非常适合用于姿态确定。然而,在陆地车辆应用中,常使用测量质量较低的低成本单频GPS接收机,并且在密集建设的城市环境中,诸如多径和低卫星可见性等外部因素会进一步降低GPS测量的质量。由于使用了低质量的接收机以及具有挑战性的城市环境,用于动态姿态确定的单历元模糊度解算成功率通常相当低。本文提出了一种微机电系统(MEMS)惯性导航系统(INS)辅助的模糊度解算方法,以提高GPS姿态确定性能,该方法特别适用于陆地车辆姿态确定。首先,用GPS载波相位和码测量对INS计算的基线向量进行增强。这改善了精度模糊度衰减因子(ADOP),从而得到质量更好的无约束浮点解。其次,使用INS辅助的模糊度函数法(AFM)进一步过滤并替换由大测量误差引起的不良浮点解。然后通过约束最小二乘模糊度去相关(CLAMBDA)算法获得固定解。最后,利用卡尔曼滤波器实现GPS/MEMS-INS集成。给出了ADOP的理论分析,实验结果表明,本文提出的方法可以显著提高浮点模糊度解的质量,从而实现高成功率和更好的姿态确定精度。

https://cdn.ncbi.nlm.nih.gov/pmc/blobs/4195/4435141/bbb90bb9498d/sensors-15-05722-g016.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/4195/4435141/7aa8ef432ab6/sensors-15-05722-g001.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/4195/4435141/f30ba8bacd0c/sensors-15-05722-g002.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/4195/4435141/8fd7e8f86f6b/sensors-15-05722-g003.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/4195/4435141/3a1eef34eb12/sensors-15-05722-g004.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/4195/4435141/84012c7a4fd9/sensors-15-05722-g005.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/4195/4435141/1a78bd828d5f/sensors-15-05722-g006.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/4195/4435141/36a176953616/sensors-15-05722-g007.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/4195/4435141/332bbc9c07fe/sensors-15-05722-g008.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/4195/4435141/4b024531071d/sensors-15-05722-g009.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/4195/4435141/e3e2afcaaf62/sensors-15-05722-g010.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/4195/4435141/e87c7799d573/sensors-15-05722-g011.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/4195/4435141/81012a2ff682/sensors-15-05722-g012.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/4195/4435141/e0888431c108/sensors-15-05722-g013.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/4195/4435141/492ff5beea8c/sensors-15-05722-g014.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/4195/4435141/5f46fadf69c9/sensors-15-05722-g015.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/4195/4435141/bbb90bb9498d/sensors-15-05722-g016.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/4195/4435141/7aa8ef432ab6/sensors-15-05722-g001.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/4195/4435141/f30ba8bacd0c/sensors-15-05722-g002.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/4195/4435141/8fd7e8f86f6b/sensors-15-05722-g003.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/4195/4435141/3a1eef34eb12/sensors-15-05722-g004.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/4195/4435141/84012c7a4fd9/sensors-15-05722-g005.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/4195/4435141/1a78bd828d5f/sensors-15-05722-g006.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/4195/4435141/36a176953616/sensors-15-05722-g007.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/4195/4435141/332bbc9c07fe/sensors-15-05722-g008.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/4195/4435141/4b024531071d/sensors-15-05722-g009.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/4195/4435141/e3e2afcaaf62/sensors-15-05722-g010.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/4195/4435141/e87c7799d573/sensors-15-05722-g011.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/4195/4435141/81012a2ff682/sensors-15-05722-g012.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/4195/4435141/e0888431c108/sensors-15-05722-g013.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/4195/4435141/492ff5beea8c/sensors-15-05722-g014.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/4195/4435141/5f46fadf69c9/sensors-15-05722-g015.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/4195/4435141/bbb90bb9498d/sensors-15-05722-g016.jpg

相似文献

1
A performance improvement method for low-cost land vehicle GPS/MEMS-INS attitude determination.一种用于低成本陆地车辆GPS/MEMS-INS姿态确定的性能改进方法。
Sensors (Basel). 2015 Mar 9;15(3):5722-46. doi: 10.3390/s150305722.
2
Performance analysis on carrier phase-based tightly-coupled GPS/BDS/INS integration in GNSS degraded and denied environments.全球导航卫星系统(GNSS)信号减弱和拒止环境下基于载波相位的紧密耦合GPS/北斗/惯性导航系统(INS)集成性能分析
Sensors (Basel). 2015 Apr 14;15(4):8685-711. doi: 10.3390/s150408685.
3
Tightly Coupled Integration of GPS Ambiguity Fixed Precise Point Positioning and MEMS-INS through a Troposphere-Constrained Adaptive Kalman Filter.通过对流层约束自适应卡尔曼滤波器实现GPS模糊度固定精密单点定位与MEMS-INS的紧密耦合集成。
Sensors (Basel). 2016 Jul 8;16(7):1057. doi: 10.3390/s16071057.
4
Implementation and Analysis of Tightly Coupled Global Navigation Satellite System Precise Point Positioning/Inertial Navigation System (GNSS PPP/INS) with Insufficient Satellites for Land Vehicle Navigation.紧耦合全球导航卫星系统精密单点定位/惯性导航系统(GNSS PPP/INS)在陆地车辆导航中卫星不足的实现与分析。
Sensors (Basel). 2018 Dec 6;18(12):4305. doi: 10.3390/s18124305.
5
Tightly-Coupled Integration of Multi-GNSS Single-Frequency RTK and MEMS-IMU for Enhanced Positioning Performance.多全球导航卫星系统单频实时动态定位与微机电惯性测量单元的紧密耦合集成以提升定位性能
Sensors (Basel). 2017 Oct 27;17(11):2462. doi: 10.3390/s17112462.
6
The inertial attitude augmentation for ambiguity resolution in SF/SE-GNSS attitude determination.用于 SF/SE-GNSS 姿态确定中模糊度解算的惯性姿态增强。
Sensors (Basel). 2014 Jun 26;14(7):11395-415. doi: 10.3390/s140711395.
7
A Low-Cost INS-Integratable GNSS Ultra-Short Baseline Attitude Determination System.低成本 INS 可集成的 GNSS 超短基线姿态确定系统。
Sensors (Basel). 2018 Jul 1;18(7):2114. doi: 10.3390/s18072114.
8
A Low-Cost, High-Precision Vehicle Navigation System for Deep Urban Multipath Environment Using TDCP Measurements.一种利用TDCP测量的适用于深度城市多径环境的低成本、高精度车辆导航系统。
Sensors (Basel). 2020 Jun 7;20(11):3254. doi: 10.3390/s20113254.
9
Implementation and Performance of a Deeply-Coupled GNSS Receiver with Low-Cost MEMS Inertial Sensors for Vehicle Urban Navigation.一种用于车辆城市导航的集成低成本MEMS惯性传感器的深度耦合GNSS接收机的实现与性能
Sensors (Basel). 2020 Jun 16;20(12):3397. doi: 10.3390/s20123397.
10
Tightly coupled low cost 3D RISS/GPS integration using a mixture particle filter for vehicular navigation.利用混合粒子滤波器实现紧密耦合低成本 3D RISS/GPS 集成,用于车辆导航。
Sensors (Basel). 2011;11(4):4244-76. doi: 10.3390/s110404244. Epub 2011 Apr 8.

引用本文的文献

1
Research on Algorithm of Airborne Dual-Antenna GNSS/MINS Integrated Navigation System.机载双天线 GNSS/MINS 组合导航系统算法研究。
Sensors (Basel). 2023 Feb 3;23(3):1691. doi: 10.3390/s23031691.
2
An Optimization Method of Ambiguity Function Based on Multi-Antenna Constrained and Application in Vehicle Attitude Determination.一种基于多天线约束的模糊函数优化方法及其在车辆姿态确定中的应用
Micromachines (Basel). 2021 Dec 30;13(1):64. doi: 10.3390/mi13010064.
3
Measurement of Unmanned Aerial Vehicle Attitude Angles Based on a Single Captured Image.

本文引用的文献

1
The inertial attitude augmentation for ambiguity resolution in SF/SE-GNSS attitude determination.用于 SF/SE-GNSS 姿态确定中模糊度解算的惯性姿态增强。
Sensors (Basel). 2014 Jun 26;14(7):11395-415. doi: 10.3390/s140711395.
2
The performance analysis of a real-time integrated INS/GPS vehicle navigation system with abnormal GPS measurement elimination.实时集成 INS/GPS 车辆导航系统的性能分析,具有异常 GPS 测量消除功能。
Sensors (Basel). 2013 Aug 15;13(8):10599-622. doi: 10.3390/s130810599.
3
Rate-gyro-integral constraint for ambiguity resolution in GNSS attitude determination applications.
基于单张拍摄图像的无人机姿态角度测量。
Sensors (Basel). 2018 Aug 13;18(8):2655. doi: 10.3390/s18082655.
4
Inclinometer Assembly Error Calibration and Horizontal Image Correction in Photoelectric Measurement Systems.光电测量系统中测斜仪组件误差校准与水平图像校正
Sensors (Basel). 2018 Jan 16;18(1):248. doi: 10.3390/s18010248.
5
Rotation Matrix Method Based on Ambiguity Function for GNSS Attitude Determination.基于模糊函数的旋转矩阵法在GNSS姿态确定中的应用
Sensors (Basel). 2016 Jun 8;16(6):841. doi: 10.3390/s16060841.
6
Coupled Integration of CSAC, MIMU, and GNSS for Improved PNT Performance.用于提升定位、导航与授时性能的CSAC、MIMU和GNSS的耦合集成
Sensors (Basel). 2016 May 12;16(5):682. doi: 10.3390/s16050682.
7
Real-time single-frequency GPS/MEMS-IMU attitude determination of lightweight UAVs.轻型无人机的实时单频全球定位系统/微机电系统惯性测量单元姿态确定
Sensors (Basel). 2015 Oct 16;15(10):26212-35. doi: 10.3390/s151026212.
8
An Adaptive Low-Cost GNSS/MEMS-IMU Tightly-Coupled Integration System with Aiding Measurement in a GNSS Signal-Challenged Environment.一种在全球导航卫星系统(GNSS)信号受挑战环境中具有辅助测量功能的自适应低成本GNSS/微机电系统惯性测量单元(MEMS-IMU)紧密耦合集成系统。
Sensors (Basel). 2015 Sep 18;15(9):23953-82. doi: 10.3390/s150923953.
9
GPS/DR Error Estimation for Autonomous Vehicle Localization.用于自动驾驶车辆定位的GPS/DR误差估计
Sensors (Basel). 2015 Aug 21;15(8):20779-98. doi: 10.3390/s150820779.
GNSS 姿态确定应用中的模糊度解算的速率-陀螺-积分约束。
Sensors (Basel). 2013 Jun 21;13(6):7979-99. doi: 10.3390/s130607979.