Satellite orbit determination by transfer with differenced ranges
文献类型:期刊论文
作者 | Yang Ying2; Li ZhiGang2; Yang XuHai2; Feng ChuGang3; Cao Fen2 |
刊名 | CHINESE SCIENCE BULLETIN
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出版日期 | 2012 |
卷号 | 57期号:36页码:4701 |
关键词 | GEOSTATIONARY SATELLITES transfer differenced ranges precise orbit determination (POD) orbit prediction |
ISSN号 | 1001-6538 |
英文摘要 | The original idea of orbit determination called "determination of satellite orbit by transfer" was proposed by the National Time Service Center, Chinese Academy of Sciences. It shows that the system is very stable and the orbit determination accuracy is improved greatly. A new observation mode called "differenced ranges between master station and slave stations by transfer" is introduced. It is the development of "determination of satellite orbit by transfer". In principle, the differenced ranges between master station and slave stations have a high angular resolution, and strongly constrains in the transverse direction of satellite orbit, perpendicular to the line-of-sight. The principle of "differenced ranges between master station and slave stations by transfer" is discussed in detail. And differenced ranges in combination with ranging data were used to determine satellite's orbit and orbit prediction under different arc observations. It shows that orbit determination accuracy for orbit prediction can be improved with differenced ranges in combination with ranging data. |
语种 | 英语 |
源URL | [http://ir.bao.ac.cn/handle/114a11/56788] ![]() |
专题 | 中国科学院国家天文台 |
作者单位 | 1.中国科学院 2.中国科学院国家授时中心 3.中国科学院国家天文台 |
推荐引用方式 GB/T 7714 | Yang Ying,Li ZhiGang,Yang XuHai,et al. Satellite orbit determination by transfer with differenced ranges[J]. CHINESE SCIENCE BULLETIN,2012,57(36):4701. |
APA | Yang Ying,Li ZhiGang,Yang XuHai,Feng ChuGang,&Cao Fen.(2012).Satellite orbit determination by transfer with differenced ranges.CHINESE SCIENCE BULLETIN,57(36),4701. |
MLA | Yang Ying,et al."Satellite orbit determination by transfer with differenced ranges".CHINESE SCIENCE BULLETIN 57.36(2012):4701. |
入库方式: OAI收割
来源:国家天文台
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