Accuracy analysis of orbit determination for high Earth orbit gravitational wave detectors using multi-GNSS sidelobe signals

IF 3.1 2区 物理与天体物理 Q1 ENGINEERING, AEROSPACE
Lisheng Tong , Kai Shao , Defeng Gu , Chengjun Yang , Chunbo Wei , Zicong An , Zheyu Xu , Jubo Zhu , Jian Wang , Daoping Liu
{"title":"Accuracy analysis of orbit determination for high Earth orbit gravitational wave detectors using multi-GNSS sidelobe signals","authors":"Lisheng Tong ,&nbsp;Kai Shao ,&nbsp;Defeng Gu ,&nbsp;Chengjun Yang ,&nbsp;Chunbo Wei ,&nbsp;Zicong An ,&nbsp;Zheyu Xu ,&nbsp;Jubo Zhu ,&nbsp;Jian Wang ,&nbsp;Daoping Liu","doi":"10.1016/j.actaastro.2025.01.022","DOIUrl":null,"url":null,"abstract":"<div><div>It is critical to maintain high-precision orbit determination in high Earth orbit gravitational wave detectors. The TianQin space-borne gravitational wave detector, a typical high Earth orbit satellite constellation, utilises an equilateral triangular satellite formation design. This paper presents the first study of the orbit determination of TianQin by utilising global navigation satellite system (GNSS) sidelobe signals through simulation. The number of visible GNSS satellites, tracking performance, position dilution of precision (PDOP), single point positioning (SPP) accuracy, and precise orbit determination (POD) accuracy of the TianQin satellites are comprehensively analysed to provide a reference for subsequent scientific tasks. The conclusions are as follows: (1) Due to the high orbit of the TianQin satellites, the signal intensity is weak, resulting in reduced visibility, narrower elevation angles of the visible antenna, and more prominent geometric accuracy factors. Therefore, utilising multi-GNSS systems and side lobe signals for orbit determination is necessary. (2) The receiver’s signal reception threshold plays a crucial role. Higher receiver sensitivity enhances the positioning and orbit determination performances of the TianQin satellites. (3) With a signal reception threshold setting of -159 dBm, the SPP accuracy of the TianQin satellites using the four GNSS system configurations is 153.81 m. (4) With a signal reception threshold set to -159 dBm, the four GNSS systems can fulfil TianQin’s orbit determination accuracy requirements of 5 m for radial position and 2 mm/s for along-track velocity within a 7-day arc length. TianQin’s position accuracy is 12.27 m for the 3-dimensional (3D) direction and 4.02 m for the radial direction, and the velocity accuracy is 0.65 mm/s for the 3D direction and 0.15 mm/s for the along-track direction.</div></div>","PeriodicalId":44971,"journal":{"name":"Acta Astronautica","volume":"229 ","pages":"Pages 534-546"},"PeriodicalIF":3.1000,"publicationDate":"2025-01-23","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Acta Astronautica","FirstCategoryId":"5","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S0094576525000244","RegionNum":2,"RegionCategory":"物理与天体物理","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q1","JCRName":"ENGINEERING, AEROSPACE","Score":null,"Total":0}
引用次数: 0

Abstract

It is critical to maintain high-precision orbit determination in high Earth orbit gravitational wave detectors. The TianQin space-borne gravitational wave detector, a typical high Earth orbit satellite constellation, utilises an equilateral triangular satellite formation design. This paper presents the first study of the orbit determination of TianQin by utilising global navigation satellite system (GNSS) sidelobe signals through simulation. The number of visible GNSS satellites, tracking performance, position dilution of precision (PDOP), single point positioning (SPP) accuracy, and precise orbit determination (POD) accuracy of the TianQin satellites are comprehensively analysed to provide a reference for subsequent scientific tasks. The conclusions are as follows: (1) Due to the high orbit of the TianQin satellites, the signal intensity is weak, resulting in reduced visibility, narrower elevation angles of the visible antenna, and more prominent geometric accuracy factors. Therefore, utilising multi-GNSS systems and side lobe signals for orbit determination is necessary. (2) The receiver’s signal reception threshold plays a crucial role. Higher receiver sensitivity enhances the positioning and orbit determination performances of the TianQin satellites. (3) With a signal reception threshold setting of -159 dBm, the SPP accuracy of the TianQin satellites using the four GNSS system configurations is 153.81 m. (4) With a signal reception threshold set to -159 dBm, the four GNSS systems can fulfil TianQin’s orbit determination accuracy requirements of 5 m for radial position and 2 mm/s for along-track velocity within a 7-day arc length. TianQin’s position accuracy is 12.27 m for the 3-dimensional (3D) direction and 4.02 m for the radial direction, and the velocity accuracy is 0.65 mm/s for the 3D direction and 0.15 mm/s for the along-track direction.
求助全文
约1分钟内获得全文 求助全文
来源期刊
Acta Astronautica
Acta Astronautica 工程技术-工程:宇航
CiteScore
7.20
自引率
22.90%
发文量
599
审稿时长
53 days
期刊介绍: Acta Astronautica is sponsored by the International Academy of Astronautics. Content is based on original contributions in all fields of basic, engineering, life and social space sciences and of space technology related to: The peaceful scientific exploration of space, Its exploitation for human welfare and progress, Conception, design, development and operation of space-borne and Earth-based systems, In addition to regular issues, the journal publishes selected proceedings of the annual International Astronautical Congress (IAC), transactions of the IAA and special issues on topics of current interest, such as microgravity, space station technology, geostationary orbits, and space economics. Other subject areas include satellite technology, space transportation and communications, space energy, power and propulsion, astrodynamics, extraterrestrial intelligence and Earth observations.
×
引用
GB/T 7714-2015
复制
MLA
复制
APA
复制
导出至
BibTeX EndNote RefMan NoteFirst NoteExpress
×
提示
您的信息不完整,为了账户安全,请先补充。
现在去补充
×
提示
您因"违规操作"
具体请查看互助需知
我知道了
×
提示
确定
请完成安全验证×
copy
已复制链接
快去分享给好友吧!
我知道了
右上角分享
点击右上角分享
0
联系我们:info@booksci.cn Book学术提供免费学术资源搜索服务,方便国内外学者检索中英文文献。致力于提供最便捷和优质的服务体验。 Copyright © 2023 布克学术 All rights reserved.
京ICP备2023020795号-1
ghs 京公网安备 11010802042870号
Book学术文献互助
Book学术文献互助群
群 号:481959085
Book学术官方微信