Low-Earth-Orbit Satellites and Robust Theory-Augmented GPS/Inertial-Navigation-System Tight Integration for Vehicle-Borne Positioning

Author:

Zhang Shixuan123,Tu Rui123,Gao Zhouzheng4ORCID,Zhang Pengfei123ORCID,Wang Siyao13,Lu Xiaochun123

Affiliation:

1. National Time Service Center, Chinese Academy of Sciences, Shu Yuan Road, Xi’an 710600, China

2. University of Chinese Academy of Sciences, Yu Quan Road, Beijing 100049, China

3. Key Laboratory of Time Reference and Applications, Chinese Academy of Sciences, Shu Yuan Road, Xi’an 710600, China

4. School of Land Science and Technology, China University of Geosciences Beijing, Beijing 100083, China

Abstract

Positioning by means of the Global Positioning System (GPS) is a traditional and widely used method. However, its performance is affected by the user environment, such as multi-path effects and poor anti-interference abilities. Therefore, an Inertial Navigation System (INS) has been integrated with GPS to overcome the disadvantages of GPS positioning. INSs do not rely on any external system information and has strong autonomy and independence from the external environment. However, the performance of GPS/INS is visibly degraded in low-observability GPS environments (tall buildings, viaducts, underground tunnels, woods, etc.). Fortunately, with the emergence of Low-Earth-Orbit (LEO) satellites in recent years, the constellation configuration can be extended with the advantages of lower orbits, greater speeds, and richer geometric structures. LEO improves the geometric structure between users and satellites and provides many more observations. Meanwhile, a robust theory approach is applied that can restrain or remove the impact of low-accuracy observations. In this study, we applied LEO data and a robust theory approach to enhance the GPS/INS tight integration. To verify the effectiveness of this method, a set of vehicles and simulated LEO data were analyzed. The results show that robust Kalman filtering (RKF) provides a visible enhancement in the positioning accuracy of GPS/INS integration. This effectively restrains the mutation error and has a smoothing effect on the positioning results. In addition, the addition of LEO data significantly improves the positioning accuracy of a sole GPS and GPS/INS integration. The GPS/LEO/INS integration has the highest positioning accuracy, with Root-Mean-Square Errors (RMSEs) of the north, east, and vertical positions of 2.38 m, 1.94 m, and 2.49 m, respectively, which corresponds to an improvement of 30.21%, 47.43%, and 34.13% compared to sole GPS-based positioning and 8.60%, 17.24%, and 12.14% when compared to the GPS/INS mode. Simultaneously, the simulation results show that LEO and INSs can improve the positioning performance of GPS under GPS-blocked conditions.

Funder

Rui Tu

Publisher

MDPI AG

Subject

Electrical and Electronic Engineering,Computer Networks and Communications,Hardware and Architecture,Signal Processing,Control and Systems Engineering

Reference43 articles.

1. Hofmann-Wellenhof, B., Lichtenegger, H., and Wasle, E. (2007). GPS-Global Navigation Satellite Systems: GPS, GLONASS, Galileo, and More, Springer Science and Bysiness Media.

2. Chai, D., Wang, S., Lu, X., and Shi, B. (2016). China Satellite Navigation Conference (CSNC) 2016 Proceedings, Springer.

3. Principles of GNSS, inertial, and multi-sensor integrated navigation systems;Groves;Ind. Robot,2013

4. Shi, E. (2012, January 18–20). An improved real-time adaptive Kalman filter for low-cost integrated GPS/INS navigation. Proceedings of the 2012 International Conference on Measurement, Information and Control, Harbin, China.

5. A Methodology for Benchmarking Real Time Kinematic GPS;Edwards;Surv. Rev.,1999

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370

www.globalauthorid.com

TOP

Copyright © 2019-2024 北京同舟云网络信息技术有限公司
京公网安备11010802033243号  京ICP备18003416号-3