JOURNAL ARTICLE

A Parallel Approach for Multi-GNSS Ultra-Rapid Orbit Determination

Chunhua JiangTianhe XuWenfeng NieZhenlong FangShuaimin WangAigong Xu

Year: 2021 Journal:   Remote Sensing Vol: 13 (17)Pages: 3464-3464   Publisher: Multidisciplinary Digital Publishing Institute

Abstract

Global Navigation Satellite System (GNSS) ultra-rapid orbit is critical for geoscience and real-time engineering applications. To improve the computational efficiency and the accuracy of predicted orbit, a parallel approach for multi-GNSS ultra-rapid orbit determination is proposed based on Message Passing Interface (MPI)/Open Multi Processing (OpenMP). This approach, compared with earlier efficient methods, can improve the efficiency of multi-GNSS ultra-rapid orbit solution without changing the original observation data and retaining the continuity and consistency of the original parameters to be estimated. To obtain high efficiency, three steps are involved in the approach. First and foremost, the normal equation construction is optimized in parallel based on MPI. Second, equivalent reduction of the estimated parameters is optimized using OpenMP parallel method. Third, multithreading is used for parallel orbit extrapolation. Thus, GNSS ultra-rapid orbit determination is comprehensively optimized in parallel, and the computation efficiency is greatly improved. Based on the data from MGEX and IGS stations, experiments are carried out to analyze the performance of the proposed approach in computational efficiency, accuracy and stability. The results show that the approach greatly improves the efficiency of satellite orbit determination. It can realize 1-h update frequency for the multi-GNSS ultra-rapid orbit determination using 88 stations with four-system observations. The accuracy of the GPS, GLONASS, Galileo and BDS ultra-rapid orbit with 1-h update frequency using the parallel approach is approximately 33.4%,31.4%,40.1% and 32.8% higher than that of the original orbit, respectively. The root mean squares (RMS) of GPS, GLONASS, Galileo and BDS predicted orbit are about 3.2 cm, 5.1 cm, 5.6 cm and 11.8 cm. Moreover, the orbit provided by the proposed method has a better stability. The precision loss of all parallel optimization can be negligible and the original correlation between the parameters is fully preserved.

Keywords:
GNSS applications Orbit determination Computer science Orbit (dynamics) Satellite Algorithm Global Positioning System Aerospace engineering Telecommunications

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FWCI (Field Weighted Citation Impact)
40
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0.83
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Citation History

Topics

GNSS positioning and interference
Physical Sciences →  Engineering →  Aerospace Engineering
Geophysics and Gravity Measurements
Physical Sciences →  Earth and Planetary Sciences →  Oceanography
Ionosphere and magnetosphere dynamics
Physical Sciences →  Physics and Astronomy →  Astronomy and Astrophysics
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