An orbit maneuver detection method based on orbital elements for BeiDou GEO and IGSO satellites

doi:10.1016/j.asr.2022.02.055

NTSC-IR > 导航与通信研究室

	An orbit maneuver detection method based on orbital elements for BeiDou GEO and IGSO satellites
	Fan, Lihong 1,2; Tu, Rui 1,2,3; Zhang, Rui 1,2; Han, Junqiang 1,2; Zhang, Pengfei 1; Wang, Siyao 1,2; Hong, Ju 1,2,3; Lu, Xiaochun 1,2,3
	2022-05-15
发表期刊	ADVANCES IN SPACE RESEARCH
ISSN	0273-1177
卷号	69 期号:10 页码:3644-3654
摘要	In addition to the orbital maneuver information, other satellite anomalies were also marked in the satellite's health status of broadcast ephemeris. For the signal-in-sp ace (SIS) performance evaluation, it is necessary to classify and evaluate the impact of a single fault, as well as the comprehensive impact. Therefore, it remains to identify the satellite orbital maneuver from the broadcast ephemeris and evaluate its impact on the signal-in-space performance. This study proposed an orbit maneuver detection method based on a combination of the square root of the major half-axis of the satellite orbit and the health status of the satellite recorded in broadcast ephemeris. The broadcast ephemerides provided by The Multi-GNSS Experiment (MGEX) from 2016 to 2020 were first used to detect the orbit maneuvers of BeiDou satellites; the orbit maneuvering and recovery periods of GEO and IGSO were detected next. The number of orbital maneuvers of the satellites made each year, and the interval of orbital maneuver of each satellite, was also obtained. The main findings of this study are as follows: (1) the proposed method can detect satellite orbit maneuvers and recovery periods recorded in the broadcast ephemeris; (2) the average orbit maneuvering interval of GEO and IGSO satellites were obtained and found to be approximately 27 days for GEO satellites except C04 and the IGSO, for which they were 45 days and approximately 178 days, respectively; (3) the average recovery time for the two types of satellite orbital maneuvers was about 6.6 h, and generally the same for the BeiDou-3 and BeiDou2 satellites; and (4) using the detected orbital maneuver intervals and recovery periods, its impact on the signal-in-space availability and continuity of the BeiDou satellite was evaluated, which showed that the per-satellite availability of IGSO satellites were approximately 0.998 and 0.9998/h respectively. The per-satellite availability of each GEO satellite was about 0.986-0.996, and the continuity was about 0.9982/h-0.9992/h; therefore, the orbital maneuver reduced the per-satellite availability and continuity of the GEO and IGSO satellites by 0.002-0.014 and approximately 0.0002/h-0.0018/h, respectively. (C)2022 COSPAR. Published by Elsevier B.V. All rights reserved.
关键词	Orbital maneuver detection Control interval of orbit maneuver Control duration of orbital maneuver Per-satellite Availability Continuity
资助者	Chinese Academy of Sciences (CAS) ; Chinese Academy of Sciences (CAS) ; National Natural Science Foundation of China ; National Natural Science Foundation of China ; National Key Research and Development Plan of China ; National Key Research and Development Plan of China ; Frontier Science Research Project ; Frontier Science Research Project ; National time service center (NTSC) programs of "Young creative talents" ; National time service center (NTSC) programs of "Young creative talents" ; Chinese Academy of Sciences (CAS) ; Chinese Academy of Sciences (CAS) ; National Natural Science Foundation of China ; National Natural Science Foundation of China ; National Key Research and Development Plan of China ; National Key Research and Development Plan of China ; Frontier Science Research Project ; Frontier Science Research Project ; National time service center (NTSC) programs of "Young creative talents" ; National time service center (NTSC) programs of "Young creative talents" ; Chinese Academy of Sciences (CAS) ; Chinese Academy of Sciences (CAS) ; National Natural Science Foundation of China ; National Natural Science Foundation of China ; National Key Research and Development Plan of China ; National Key Research and Development Plan of China ; Frontier Science Research Project ; Frontier Science Research Project ; National time service center (NTSC) programs of "Young creative talents" ; National time service center (NTSC) programs of "Young creative talents" ; Chinese Academy of Sciences (CAS) ; Chinese Academy of Sciences (CAS) ; National Natural Science Foundation of China ; National Natural Science Foundation of China ; National Key Research and Development Plan of China ; National Key Research and Development Plan of China ; Frontier Science Research Project ; Frontier Science Research Project ; National time service center (NTSC) programs of "Young creative talents" ; National time service center (NTSC) programs of "Young creative talents"
DOI	10.1016/j.asr.2022.02.055
关键词[WOS]	ROBUST METHOD ; SYSTEM ; PERFORMANCE
语种	英语
资助项目	Chinese Academy of Sciences (CAS)[Y916YRa701] ; Chinese Academy of Sciences (CAS)[E017YR1R04] ; Chinese Academy of Sciences (CAS)[E123YR1R03] ; Chinese Academy of Sciences (CAS)[Y923YC1701] ; National Natural Science Foundation of China[41674034] ; National Natural Science Foundation of China[41974032] ; National Key Research and Development Plan of China[2016YFB0501804] ; Frontier Science Research Project[QYZDB-SSW-DQC028] ; National time service center (NTSC) programs of "Young creative talents"[Y824SC1S06]
资助者	Chinese Academy of Sciences (CAS) ; Chinese Academy of Sciences (CAS) ; National Natural Science Foundation of China ; National Natural Science Foundation of China ; National Key Research and Development Plan of China ; National Key Research and Development Plan of China ; Frontier Science Research Project ; Frontier Science Research Project ; National time service center (NTSC) programs of "Young creative talents" ; National time service center (NTSC) programs of "Young creative talents" ; Chinese Academy of Sciences (CAS) ; Chinese Academy of Sciences (CAS) ; National Natural Science Foundation of China ; National Natural Science Foundation of China ; National Key Research and Development Plan of China ; National Key Research and Development Plan of China ; Frontier Science Research Project ; Frontier Science Research Project ; National time service center (NTSC) programs of "Young creative talents" ; National time service center (NTSC) programs of "Young creative talents" ; Chinese Academy of Sciences (CAS) ; Chinese Academy of Sciences (CAS) ; National Natural Science Foundation of China ; National Natural Science Foundation of China ; National Key Research and Development Plan of China ; National Key Research and Development Plan of China ; Frontier Science Research Project ; Frontier Science Research Project ; National time service center (NTSC) programs of "Young creative talents" ; National time service center (NTSC) programs of "Young creative talents" ; Chinese Academy of Sciences (CAS) ; Chinese Academy of Sciences (CAS) ; National Natural Science Foundation of China ; National Natural Science Foundation of China ; National Key Research and Development Plan of China ; National Key Research and Development Plan of China ; Frontier Science Research Project ; Frontier Science Research Project ; National time service center (NTSC) programs of "Young creative talents" ; National time service center (NTSC) programs of "Young creative talents"
WOS研究方向	Engineering ; Astronomy & Astrophysics ; Geology ; Meteorology & Atmospheric Sciences
WOS类目	Engineering, Aerospace ; Astronomy & Astrophysics ; Geosciences, Multidisciplinary ; Meteorology & Atmospheric Sciences
WOS记录号	WOS:000795158600007
出版者	ELSEVIER SCI LTD
引用统计
文献类型	期刊论文
条目标识符	http://210.72.145.45/handle/361003/13820
专题	导航与通信研究室
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 Precis Nav Positioning & Timing Technol, Shu Yuan Rd, Xian 710600, Peoples R China 3.Univ Chinese Acad Sci, Yu Quan Rd, Beijing 100049, Peoples R China
推荐引用方式 GB/T 7714	Fan, Lihong,Tu, Rui,Zhang, Rui,et al. An orbit maneuver detection method based on orbital elements for BeiDou GEO and IGSO satellites[J]. ADVANCES IN SPACE RESEARCH,2022,69(10):3644-3654.
APA	Fan, Lihong.,Tu, Rui.,Zhang, Rui.,Han, Junqiang.,Zhang, Pengfei.,...&Lu, Xiaochun.(2022).An orbit maneuver detection method based on orbital elements for BeiDou GEO and IGSO satellites.ADVANCES IN SPACE RESEARCH,69(10),3644-3654.
MLA	Fan, Lihong,et al."An orbit maneuver detection method based on orbital elements for BeiDou GEO and IGSO satellites".ADVANCES IN SPACE RESEARCH 69.10(2022):3644-3654.