anewmethodfordeterminationofsatelliteorbitsbytransfer
文献类型：期刊论文
| 作者 | LI ZhiGang3 ; YANG XuHai3; AI GuoXiang2; SI HuLi2; QIAO RongChuan3; FENG ChuGang1
|
| 刊名 | scienceinchinaseriesgphysicsmechanicsastronomy
 |
| 出版日期 | 2009 |
| 卷号 | 52期号:3页码:384 |
| ISSN号 | 1672-1799 |
| 英文摘要 | The original idea of a new method for determination of satellite orbits by transfer is from Two-Way Satellite Time and Frequency Transfer (TWSTFT). The original method is called "determination of satellite orbit by transfer". The method is not only for determination of satellite orbit but also for the time transfer with high accuracy and precision. The advantage is that the accuracy and the precision for determination of satellite orbit are very high and the new method is favorable for various applications. The combination of various signals disseminated and received forms various modes of satellite orbit determinations. If receivers at stations receive the own station-disseminated signals via a satellite transponder, it forms an orbit determination mode called "receiving the own station-disseminated signals mode". If receivers at all stations receive the signals disseminated from the master station via satellite transponders, it forms an orbit determination mode called "receiving the master station-disseminated signals mode". If all of receivers at stations receive all stations-disseminated signals via satellite transponders, it forms an orbit determination mode called "receiving all stations-disseminated signals mode". Also there are other combinations of signals for satellite orbit determination. For different orbit determination modes with different signal combinations, their rigorous formulae of processing are hereby presented in this paper. The accurate and the precise satellite orbit determination for both of the modes, "receiving the own station-disseminated signals mode" and "receiving the master station-disseminated signals mode" is attempted. It shows that the accuracy and precision for both of modes are nearly the same, the ranging accuracy is better than 1 cm, and the observation residuals of satellite orbit determination are better than 9 cm in the observation duration of 1 day. |
| 资助项目 | [National Basic Research and Development Program of China] |
| 语种 | 英语 |
| 源URL | [http://210.72.145.45/handle/361003/9774]  |
| 专题 | 国家授时中心_高精度时间传递与精密测定轨研究室 |
| 作者单位 | 1.中国科学院上海天文台 2.中国科学院南京天文光学技术研究所 3.中国科学院国家授时中心 |
| 推荐引用方式 GB/T 7714 | LI ZhiGang,YANG XuHai,AI GuoXiang,et al. anewmethodfordeterminationofsatelliteorbitsbytransfer[J]. scienceinchinaseriesgphysicsmechanicsastronomy,2009,52(3):384. |
| APA | LI ZhiGang,YANG XuHai,AI GuoXiang,SI HuLi,QIAO RongChuan,&FENG ChuGang.(2009).anewmethodfordeterminationofsatelliteorbitsbytransfer.scienceinchinaseriesgphysicsmechanicsastronomy,52(3),384. |
| MLA | LI ZhiGang,et al."anewmethodfordeterminationofsatelliteorbitsbytransfer".scienceinchinaseriesgphysicsmechanicsastronomy 52.3(2009):384. |
入库方式： OAI收割
来源：国家授时中心
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