Real-Time Detection of Orbital Maneuvers Using Epoch-Differenced Carrier Phase Observations and Broadcast Ephemeris Data: A Case Study of the BDS Dataset

The orbital maneuvers of the global navigation satellite system (GNSSs) have a significant influence on the performance of the precise positioning, navigation, and timing (PNT) services. Because the Chinese BeiDou Navigation Satellite System (BDS) has three types of satellites in the geostationary o...

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Main Authors: Rui Tu, Rui Zhang, Lihong Fan, Junqiang Han, Pengfei Zhang, Xiaochun Lu
Format: Article
Language:English
Published: MDPI AG 2020-08-01
Series:Sensors
Subjects:
Online Access:https://www.mdpi.com/1424-8220/20/16/4584
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author Rui Tu
Rui Zhang
Lihong Fan
Junqiang Han
Pengfei Zhang
Xiaochun Lu
author_facet Rui Tu
Rui Zhang
Lihong Fan
Junqiang Han
Pengfei Zhang
Xiaochun Lu
author_sort Rui Tu
collection DOAJ
description The orbital maneuvers of the global navigation satellite system (GNSSs) have a significant influence on the performance of the precise positioning, navigation, and timing (PNT) services. Because the Chinese BeiDou Navigation Satellite System (BDS) has three types of satellites in the geostationary orbit (GEO), inclined geosynchronous orbit (IGSO), and medium earth orbit (MEO) maneuvers occur more frequently. Thus, it is essential to determine an effective approach for the detection of orbital maneuvers. This study proposes a method for the detection of orbital maneuvers using epoch-differenced carrier phase observations and broadcast ephemeris data. When using the epoch-differenced velocity estimation as a basic data solution model, the time discrimination and satellite identification factors are defined and used for the real-time detection of the beginning and the pseudorandom noise code (PRN) of satellites. The datasets from four GNSS stations (WUH1, BJF1, POHN, CUT0) from the year 2016 were collected and analyzed. The validations showed that the beginning, the PRN of the orbital maneuver of the satellite can be precisely detected in real time for all GEO, IGSO, and MEO satellites, and the detected results also showed good consistency, with the beginning time at a difference of 1–2 min across different stations. The proposed approach was observed to be more sensitive, and the detected beginning time was about 30 min earlier than the single point positioning approach when the high-precision carrier phase observation was used. Thus, orbital maneuvering can be accurately detected by the proposed method. It not only improves the utilization of the collected data but also improves the performance of PNT services.
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spelling doaj.art-d9b1a7df44c243a481d58a1e3884c33e2023-11-20T10:16:15ZengMDPI AGSensors1424-82202020-08-012016458410.3390/s20164584Real-Time Detection of Orbital Maneuvers Using Epoch-Differenced Carrier Phase Observations and Broadcast Ephemeris Data: A Case Study of the BDS DatasetRui Tu0Rui Zhang1Lihong Fan2Junqiang Han3Pengfei Zhang4Xiaochun Lu5National Time Service Center, Chinese Academy of Sciences, Shu Yuan Road, Xi’an 710600, ChinaNational Time Service Center, Chinese Academy of Sciences, Shu Yuan Road, Xi’an 710600, ChinaNational Time Service Center, Chinese Academy of Sciences, Shu Yuan Road, Xi’an 710600, ChinaNational Time Service Center, Chinese Academy of Sciences, Shu Yuan Road, Xi’an 710600, ChinaNational Time Service Center, Chinese Academy of Sciences, Shu Yuan Road, Xi’an 710600, ChinaNational Time Service Center, Chinese Academy of Sciences, Shu Yuan Road, Xi’an 710600, ChinaThe orbital maneuvers of the global navigation satellite system (GNSSs) have a significant influence on the performance of the precise positioning, navigation, and timing (PNT) services. Because the Chinese BeiDou Navigation Satellite System (BDS) has three types of satellites in the geostationary orbit (GEO), inclined geosynchronous orbit (IGSO), and medium earth orbit (MEO) maneuvers occur more frequently. Thus, it is essential to determine an effective approach for the detection of orbital maneuvers. This study proposes a method for the detection of orbital maneuvers using epoch-differenced carrier phase observations and broadcast ephemeris data. When using the epoch-differenced velocity estimation as a basic data solution model, the time discrimination and satellite identification factors are defined and used for the real-time detection of the beginning and the pseudorandom noise code (PRN) of satellites. The datasets from four GNSS stations (WUH1, BJF1, POHN, CUT0) from the year 2016 were collected and analyzed. The validations showed that the beginning, the PRN of the orbital maneuver of the satellite can be precisely detected in real time for all GEO, IGSO, and MEO satellites, and the detected results also showed good consistency, with the beginning time at a difference of 1–2 min across different stations. The proposed approach was observed to be more sensitive, and the detected beginning time was about 30 min earlier than the single point positioning approach when the high-precision carrier phase observation was used. Thus, orbital maneuvering can be accurately detected by the proposed method. It not only improves the utilization of the collected data but also improves the performance of PNT services.https://www.mdpi.com/1424-8220/20/16/4584BDSorbital maneuverscarrier phase observationvelocity estimationepoch-difference
spellingShingle Rui Tu
Rui Zhang
Lihong Fan
Junqiang Han
Pengfei Zhang
Xiaochun Lu
Real-Time Detection of Orbital Maneuvers Using Epoch-Differenced Carrier Phase Observations and Broadcast Ephemeris Data: A Case Study of the BDS Dataset
Sensors
BDS
orbital maneuvers
carrier phase observation
velocity estimation
epoch-difference
title Real-Time Detection of Orbital Maneuvers Using Epoch-Differenced Carrier Phase Observations and Broadcast Ephemeris Data: A Case Study of the BDS Dataset
title_full Real-Time Detection of Orbital Maneuvers Using Epoch-Differenced Carrier Phase Observations and Broadcast Ephemeris Data: A Case Study of the BDS Dataset
title_fullStr Real-Time Detection of Orbital Maneuvers Using Epoch-Differenced Carrier Phase Observations and Broadcast Ephemeris Data: A Case Study of the BDS Dataset
title_full_unstemmed Real-Time Detection of Orbital Maneuvers Using Epoch-Differenced Carrier Phase Observations and Broadcast Ephemeris Data: A Case Study of the BDS Dataset
title_short Real-Time Detection of Orbital Maneuvers Using Epoch-Differenced Carrier Phase Observations and Broadcast Ephemeris Data: A Case Study of the BDS Dataset
title_sort real time detection of orbital maneuvers using epoch differenced carrier phase observations and broadcast ephemeris data a case study of the bds dataset
topic BDS
orbital maneuvers
carrier phase observation
velocity estimation
epoch-difference
url https://www.mdpi.com/1424-8220/20/16/4584
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