Abstract

The frequent maneuvering of BeiDou Geostationary Orbit (GEO) and Inclined Geosynchronous Orbit (IGSO) satellites affects the availability of real-time orbit, and decreases the accuracy and performance of positioning, navigation and time (PNT) services. BeiDou satellite maneuver information cannot be obtained by common users. BeiDou broadcast ephemeris is the only indicator of the health status of satellites, which are broadcast on an hourly basis, easily leading to ineffective observations. Sometimes, identification errors of satellite abnormity also appear in the broadcast ephemeris. This study presents a real-time robust detection method for a satellite orbital maneuver with high frequency and high reliability. By using the broadcast ephemeris and pseudo-range observations, the time discrimination factor and the satellite identification factor were defined and used for the real-time detection of start time and the pseudo-random noise code (PRN) of satellites was used for orbital maneuvers. Data from a Multi-GNSS Experiment (MGEX) was collected and analyzed. The results show that the start time and the PRN of the satellite orbital maneuver could be detected accurately in real time. In addition, abnormal start times and satellite abnormities caused by non-maneuver factors also could be detected using the proposed method. The new method not only improves the utilization of observations for users with the data effective for about 92 min, but also promotes the reliability of real-time PNT services.

Highlights

  • Since 27 December 2012, the BeiDou-2 regional navigation system has provided regional positioning, navigation and timing (PNT) services across the Asia-Pacific region

  • Du et al monitored the orbital maneuver of the BeiDou Geostationary Orbit (GEO) satellite using the orbit measurement data of the China Area Positioning System (CAPS), CAPS measurements are not available to common users [22]

  • In order to solve the above problems, this study presents a robust real-time detection method for the satellite orbital maneuver only by using the broadcast ephemeris and the pseudo-range observations of a single BeiDou Navigation Satellite System (BDS) receiver

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Summary

Introduction

Since 27 December 2012, the BeiDou-2 regional navigation system has provided regional positioning, navigation and timing (PNT) services across the Asia-Pacific region. Yan et al analyzed a method to detect the maneuvering satellite using the restored orbit from the broadcast ephemeris of the BeiDou Navigation Satellite System (BDS) [19]. Du et al monitored the orbital maneuver of the BeiDou GEO satellite using the orbit measurement data of the China Area Positioning System (CAPS), CAPS measurements are not available to common users [22]. In order to solve the above problems, this study presents a robust real-time detection method for the satellite orbital maneuver only by using the broadcast ephemeris and the pseudo-range observations of a single BDS receiver. The proposed method, which does not need any additional data information and the orbit force model, can detect the orbital maneuver and orbital abnormities simultaneously, in real time. The proposed method benefits both static and dynamic positioning users

Materials and Methods
Time Discriminant Factor of Satellite Orbit Maneuver
The Satellite Identification Factor of Satellite Orbital Maneuver
Robust Equivalent Weight Matrix of the Observations
The Selection of Empirical Threshold
Data Description
Orbital Maneuver Detection for GEO
The time factor factor of the the orbital maneuver maneuver for XMIS
The health status of box
The between pseudo-range SPP
Another Application of the Detected Method
The Application of the Detected Method for other GNSS MEO Constellations
By orbits comparing with
Conclusions and Discussion
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