Abstract

An n-station continuously operated global navigation satellite system (GNSS) network contains n-1 independent baselines. Baseline structure is critical to positioning accuracy, and the final result is dependent on the baseline selection strategies. The baseline length and amount of common observations are the primary principles for baseline selection. However, there are few discussions about the optimal strategy to determine the independent baseline of a huge GNSS network. To enhance the performance of the multibaseline solution, a comparison is drawn between the conventional method and a weighting strategy. Observations from continuous stations distributed globally within the International GNSS Service (IGS) are explored. At first, two conventional principles for baseline selection are tested. Subsequently, a weighting scheme is developed to exploit these two strategies. The enhanced method improves nearly 10% external accuracy compared with the classical methods, which can be verified from the experiment on January 1, 2012. Lastly, the network experiment is extended to the whole year of 2012 to increase statistical significance. It is therefore revealed that the novel weighting strategy (WEIGHT), with an equal chance of two conventional strategies, mitigates 0.4%–3.0% three-dimensional (3D) coordinate error of the whole year. Also, an analysis of the probability of gross errors indicates that WEIGHT exhibits better performance. Unlike the conventional view, it is shown that a proper weight of OBS-MAX and SHORTEST could form a better coordinate calculation result and a lower gross error rate. In conclusion, these experiments suggest a proposed method that synthetically considers the length of total stations and the total number of observations, and it is verified that WEIGHT is a better choice for searching independent baselines.

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Data Availability Statement

Some or all data, models, or code that support the findings of this study are available from the corresponding author upon reasonable request.
The specific data that is available upon request:
1.
All the source RINEX file and result files from January 1, 2012;
2.
The 1-year coordinate result files of different strategies; and
3.
The code for the minimum spanning tree.

Acknowledgments

Funding from Harbin Institute of Technology at Shenzhen and Shandong University at Weihai is gratefully acknowledged. This work is supported by the Shenzhen science and technology program (Group No. KQTD20180410161218820). This work is supported by the National Key Research Program of China “Collaborative Precision Positioning Project” (No. 2016YFB0501900). Grateful acknowledgement is made to those who helped with this research: Prof. Dagang Ye from National Taipei University (NTPU) provided help with software; the editor and three anonymous reviewers gave heuristic advice and detailed correction. The numerical calculation in this paper is finished based on the supercomputing system in the Supercomputing Center, Shandong University at Weihai.

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Go to Journal of Surveying Engineering
Journal of Surveying Engineering
Volume 147Issue 1February 2021

History

Received: Dec 29, 2019
Accepted: Jul 10, 2020
Published online: Oct 16, 2020
Published in print: Feb 1, 2021
Discussion open until: Mar 16, 2021

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Ph.D. Student, Research Building, Harbin Institute of Technology at Shenzhen, Taoyuan St., Nanshan District, Shenzhen, Guangdong Province 518055, China. Email: [email protected]
Professor, School of Space Science and Physics, Shandong Univ. at Weihai, Wenhua West Rd., Weihai, Shandong Province 264209, China. ORCID: https://orcid.org/0000-0001-5818-6264. Email: [email protected]
Wenfeng Nie [email protected]
Associate Research Fellow, Interdisciplinary Div. of Aeronautical and Aviation Engineering Hong Kong Polytechnic Univ., Number 11, Yucai Rd., Hung Hom, Kowloon 999077, Hong Kong. Email: [email protected]
Ph.D. Student, School of Space Science and Physics, Shandong Univ. at Weihai, Wenhua West Rd., Weihai, Shandong Province 264209, China. Email: [email protected]
Zhenlong Fang [email protected]
Ph.D. Student, School of Space Science and Physics, Shandong Univ. at Weihai, Wenhua West Rd., Weihai, Shandong Province 264209, China. Email: [email protected]
Postdoctoral Researcher, School of Space Science and Physics, Shandong Univ. at Weihai, Wenhua West Rd., Weihai, Shandong Province 264209, China. Email: [email protected]
Yiping Jiang [email protected]
Assistant Professor, Interdisciplinary Div. of Aeronautical and Aviation Engineering, Hong Kong Polytechnic Univ., Number 11, Yucai Rd., Hung Hom, Kowloon 999077, Hong Kong. Email: [email protected]
Guochang Xu [email protected]
Professor, Institute of Space Science and Applied Technology, Harbin Institute of Technology at Shenzhen, Taoyuan St., Nanshan District, Shenzhen, Guangdong Province 518055, China (corresponding author). Email: [email protected]

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