Precision Orbit Determination Based on Single Stations Laser Ranging Observation
In the process of Satellite Laser Ranging (SLR), besides recording the time transit of the laser beam between the station and the satellite, it also records the tele scopes direction at the laser fire epoch. That is, (t,Δt, A, h) can be acquired by SLR, where Δt is associated to the range. For cooperating objects, multi-stations SLR data can be easily obtained; for non-cooperating objects, it is difficult or even impossible. So it is worthy to discuss how to determinate orbit just using single stations SLR data, which is the core object of this article. Additionally, it can be used to estimate some parameters of the SLR system, like alignment between the fire light axis and the telescopes main axis. And it is very convenient to estimate the precision of cooperating objects determined orbit, so that easily improving the method.
SLR Observation Precision Orbit Determination Synthesis Single Station
Rongwang Li Hesheng Feng Yuqiang Li Yaoheng Xiong
National Astronomical Observations / Yunnan Observatory, Chinese Academy of Sciences, Kunming 65001 National Astronomical Observations / Yunnan Observatory, Chinese Academy of Sciences, Kunming 65001
国际会议
The 10th Asian-Pacific Regional International Astronomical Union Meeting(第十届亚洲及太平洋地区天文学大会 APRIM)
昆明
英文
364-365
2008-08-03（万方平台首次上网日期，不代表论文的发表时间）