期刊文献+

USB与VLBI联合确定“探测一号”卫星轨道 被引量:13

Joint Orbit Determination for TC-1 Satellite with USB and VLBI
下载PDF
导出
摘要 我国绕月探测工程“嫦娥一号”卫星将以统一S波段(USB)为主,辅以甚长基线干涉仪(VLBI)测轨分系统来完成测控任务。由于“探测一号”卫星轨道与“嫦娥一号”调相轨道段相似,有关单位于2005年3月17日-20日进行了USB和VLBI联合跟踪“探测一号”试验。通过对联合测轨数据的处理,研究了USB—VLBI联合定轨方法,分析了联合定轨和预报精度,得出了一些结论。 Chang'E-1, China's first lunar exploration project, will mainly make use of a Unified S-Band (USB) TT&C network to provide measurement and control of the spacecraft with Very Long Baseline Interferometry (VLBI) as a complement. Because the orbit of TC-1 satellite is similar to Chang'E-1's phasing orbit, the test on USB and VLBrs joint tracking of TC-1 was carried out in China on March 17-20, 2005. Through data processing, we investigated the method of orbit determination by combining USB and VLBI, analyzed the precision of orbit determination and orbit prediction, and came up with a useful conclusion.
出处 《飞行器测控学报》 2006年第1期31-36,共6页 Journal of Spacecraft TT&C Technology
关键词 统一S波段系统(USB) 甚长基线干涉仪(VLBI) 探测一号 联合轨道确定 时延 USB VLBI TC-1 Joint Orbit Determination Time Delay
  • 相关文献

参考文献6

  • 1李济生.人造卫星精密轨道确定[M].北京:解放军出版社,1995.. 被引量:102
  • 2刘林著..航天器轨道理论[M].北京:国防工业出版社,2000:621.
  • 3Gruber Th,Bode A,Reigber C,et al. GRIM5-C1: Combination solution of the global gravity field to degree and order 120[J]. Geophysics Research Letters, 2000,27(24): 4005-4008. 被引量:1
  • 4Berger C, Biancale R,Ill M,et al. Improvements of the empirical thermospheric model DTM:DTM94-a comparative review of various temporal variations and prospects in space geodesy applications[J].J. Geod.,1998, 72(3):161-178. 被引量:1
  • 5McCarthy D D (Editor). IERS Conventions[R]. IERS Technical Note 21, 1996. 被引量:1
  • 6Ray R D. A global ocean tide model from TOPEX/Poseidon altimetry: GOT99.2[R]. NASA Tech. Memo. 209478, Goddard Space Flight Center, 1999. 被引量:1

共引文献101

同被引文献104

引证文献13

二级引证文献80

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部