Abstract

The rapid movement of low Earth orbit (LEO) satellite can improve geometric diversity, which contributes to the rapid convergence of Global Navigation Satellite System (GNSS) precise point positioning (PPP). However, the LEO onboard receiver clock cannot be used directly by PPP users as the LEO satellite clock because the LEO onboard receiver clock and LEO satellite clock absorb different code delays when receiving and transmitting signals. In this study, a real-time estimation approach for the LEO satellite clock based on ground tracking stations was proposed for the first time. The feasibility for the rapid convergence of the LEO satellite clock was analyzed using the satellite time dilution of precision (TDOP) that one satellite is relative to multiple ground tracking stations. The LEO constellation of 168 satellites and observations for 15 ground tracking stations were simulated to verify the proposed method. The experiment results showed that the average convergence time was 31.21 min for the Global Positioning System (GPS) satellite clock, whereas the value for the LEO satellite clock was only 2.86 min. The average root mean square (RMS) and standard deviation (STD) values after convergence were 0.71 and 0.39 ns for the LEO satellite clock, whereas the values were 0.31 and 0.13 ns for the GPS satellite clock. The average weekly satellite TDOP for the LEO satellite was much smaller than that for the GPS satellite. The average satellite TDOPs for all LEO and GPS satellites were 19.13 and 1294.70, respectively. However, the average delta TDOPs caused by satellite motion for all LEO and GPS satellites were both 0.10. Therefore, the rapid convergence of the LEO satellite clock resulted from the better geometric distribution of the LEO satellite relative to ground stations. Despite errors and the convergence time of the LEO satellite clock, the convergence time and positioning accuracy for LEO-augmented GPS and BeiDou Navigation Satellite System (BDS) PPP with the real-time estimated LEO satellite clock can still reach 10.63 min, 1.94 cm, 1.44 cm, and 4.18 cm in the east, north, and up components, respectively. The improvements caused by LEO satellite for GPS/BDS PPP were 59%, 30%, 31%, and 33%, respectively.

Highlights

  • As an absolute positioning technology suitable for large areas with high precision, precise point positioning (PPP) has developed into one of the most representative technologies in Global Navigation Satellite System (GNSS) precise positioning [1]

  • The feasibility for the rapid convergence of the low Earth orbit (LEO) satellite clock was evaluated using the satellite time dilution of precision (TDOP) that one satellite is relative to multiple ground tracking stations

  • We calculated the number of ground tracking stations where one satellite could be observed, satellite TDOP that one satellite is relative to multiple ground tracking stations, to further analyze the reason for the rapid convergence of the LEO satellite clock

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Summary

Introduction

As an absolute positioning technology suitable for large areas with high precision, precise point positioning (PPP) has developed into one of the most representative technologies in Global Navigation Satellite System (GNSS) precise positioning [1]. Multi-GNSS has great potential to improve the performance of PPP considerably, and the convergence time and positioning accuracy can be improved by approximately 70% and 25% compared with that of Global Positioning System (GPS) [2,3,5]. The geometry change of the GNSS satellite relative to the ground station is excessively slow, such that approximately 20 minutes are required to complete the PPP convergence process due to the high orbit altitude [4,7]. These problems of GNSS PPP limit its adoption in time-critical applications, especially in real-time applications [8]. How to improve the convergence time of multi-GNSS PPP dramatically remains an urgent problem to be solved

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