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

doi:10.3390/s20164584

NTSC-IR

	Real-Time Detection of Orbital Maneuvers Using Epoch-Differenced Carrier Phase Observations and Broadcast Ephemeris Data: A Case Study of the BDS Dataset
	Tu, Rui 1,2,3; Zhang, Rui 1,2; Fan, Lihong 1,2; Han, Junqiang 1,2; Zhang, Pengfei 1,2; Lu, Xiaochun1,2,3
	2020-08-01
发表期刊	SENSORS
卷号	20 期号:16 页码:17
摘要	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.
关键词	BDS orbital maneuvers carrier phase observation velocity estimation epoch-difference
资助者	National Natural Science Foundation of China ; National Natural Science Foundation of China ; Chinese Academy of Science (CAS) ; Chinese Academy of Science (CAS) ; National Natural Science Foundation of China ; National Natural Science Foundation of China ; Chinese Academy of Science (CAS) ; Chinese Academy of Science (CAS) ; National Natural Science Foundation of China ; National Natural Science Foundation of China ; Chinese Academy of Science (CAS) ; Chinese Academy of Science (CAS) ; National Natural Science Foundation of China ; National Natural Science Foundation of China ; Chinese Academy of Science (CAS) ; Chinese Academy of Science (CAS)
DOI	10.3390/s20164584
关键词[WOS]	SATELLITE ; BEIDOU ; PERFORMANCE ; NAVIGATION ; GPS ; PPP
语种	英语
资助项目	National Natural Science Foundation of China[41674034] ; National Natural Science Foundation of China[41974032] ; National Natural Science Foundation of China[11903040] ; Chinese Academy of Science (CAS)[Y923YC1701] ; Chinese Academy of Science (CAS)[QYZDB-SSW-DQC028]
资助者	National Natural Science Foundation of China ; National Natural Science Foundation of China ; Chinese Academy of Science (CAS) ; Chinese Academy of Science (CAS) ; National Natural Science Foundation of China ; National Natural Science Foundation of China ; Chinese Academy of Science (CAS) ; Chinese Academy of Science (CAS) ; National Natural Science Foundation of China ; National Natural Science Foundation of China ; Chinese Academy of Science (CAS) ; Chinese Academy of Science (CAS) ; National Natural Science Foundation of China ; National Natural Science Foundation of China ; Chinese Academy of Science (CAS) ; Chinese Academy of Science (CAS)
WOS研究方向	Chemistry ; Engineering ; Instruments & Instrumentation
WOS类目	Chemistry, Analytical ; Engineering, Electrical & Electronic ; Instruments & Instrumentation
WOS记录号	WOS:000564709800001
出版者	MDPI
引用统计
文献类型	期刊论文
条目标识符	http://210.72.145.45/handle/361003/9387
专题	中国科学院国家授时中心
通讯作者	Tu, Rui
作者单位	1.Chinese Acad Sci, Natl Time Serv Ctr, Shu Yuan Rd, Xian 710600, Peoples R China 2.Chinese Acad Sci, Key Lab Time & Frequency Primary Stand, Xian 710600, Peoples R China 3.Univ Chinese Acad Sci, Sch Astron & Space Sci, Yu Quan Rd, Beijing 100049, Peoples R China
推荐引用方式 GB/T 7714	Tu, Rui,Zhang, Rui,Fan, Lihong,et al. Real-Time Detection of Orbital Maneuvers Using Epoch-Differenced Carrier Phase Observations and Broadcast Ephemeris Data: A Case Study of the BDS Dataset[J]. SENSORS,2020,20(16):17.
APA	Tu, Rui,Zhang, Rui,Fan, Lihong,Han, Junqiang,Zhang, Pengfei,&Lu, Xiaochun.(2020).Real-Time Detection of Orbital Maneuvers Using Epoch-Differenced Carrier Phase Observations and Broadcast Ephemeris Data: A Case Study of the BDS Dataset.SENSORS,20(16),17.
MLA	Tu, Rui,et al."Real-Time Detection of Orbital Maneuvers Using Epoch-Differenced Carrier Phase Observations and Broadcast Ephemeris Data: A Case Study of the BDS Dataset".SENSORS 20.16(2020):17.