An orbit maneuver detection method based on orbital elements for BeiDou GEO and IGSO satellites
文献类型：期刊论文
| 作者 | Fan, Lihong2,3; Tu, Rui1,2,3; Zhang, Rui2,3; Han, Junqiang2,3; Zhang, Pengfei3; Wang, Siyao2,3; Hong, Ju1,2,3; Lu, Xiaochun1,2,3 |
| 刊名 | ADVANCES IN SPACE RESEARCH
 |
| 出版日期 | 2022-05-15 |
| 卷号 | 69期号:10页码:3644-3654 |
| 关键词 | Orbital maneuver detection Control interval of orbit maneuver Control duration of orbital maneuver Per-satellite Availability Continuity |
| ISSN号 | 0273-1177 |
| DOI | 10.1016/j.asr.2022.02.055 |
| 英文摘要 | 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. |
| WOS关键词 | ROBUST METHOD ; SYSTEM ; PERFORMANCE |
| 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] |
| WOS研究方向 | Engineering ; Astronomy & Astrophysics ; Geology ; Meteorology & Atmospheric Sciences |
| 语种 | 英语 |
| WOS记录号 | WOS:000795158600007 |
| 出版者 | ELSEVIER SCI LTD |
| 资助机构 | 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" |
| 源URL | [http://210.72.145.45/handle/361003/13820]  |
| 专题 | 国家授时中心_导航与通信研究室 |
| 通讯作者 | Tu, Rui |
| 作者单位 | 1.Univ Chinese Acad Sci, Yu Quan Rd, Beijing 100049, Peoples R China 2.Chinese Acad Sci, Key Lab Precis Nav Positioning & Timing Technol, Shu Yuan Rd, Xian 710600, Peoples R China 3.Chinese Acad Sci, Natl Time Serv Ctr, Shu Yuan Rd, Xian 710600, 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. |
入库方式： OAI收割
来源：国家授时中心
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