中国科学院机构知识库网格
Chinese Academy of Sciences Institutional Repositories Grid
The application of the instantaneous states reduction to the orbital monitoring of pivotal arcs of the Chang'E-1 satellite

文献类型:期刊论文

作者Li JinLing; Guo Li; Qian ZhiHan; Ping JinSong
刊名SCIENCE IN CHINA SERIES G-PHYSICS MECHANICS & ASTRONOMY
出版日期2009-12-01
卷号52期号:12页码:1833-1841
关键词lunar exploration orbital maneuver trace monitoring instantaneous states CE-1 satellite
英文摘要In the Chinese lunar exploration project, the Chang'E-1 (CE-1) satellite was jointly monitored by the United S-band range and Doppler and the VLBI technique. A real-time reduction of the tracking data is realized to deduce the time series of the instantaneous state vectors (ISV) (position and velocity vectors) of the CE-1 satellite, and is applied to the orbital monitoring of pivotal arcs. This paper introduces this real-time data reduction method and its application to the orbital monitoring of pivotal arcs of the CE-1 satellite in order to serve as a source of criticism and reference.
WOS标题词Science & Technology ; Physical Sciences
类目[WOS]Physics, Multidisciplinary
研究领域[WOS]Physics
收录类别SCI
语种英语
WOS记录号WOS:000272622300004
源URL[http://119.78.226.72/handle/331011/19572]  
专题上海天文台_天文地球动力学研究中心
作者单位Shanghai Astron Observ, Shanghai 200030, Peoples R China
推荐引用方式
GB/T 7714
Li JinLing,Guo Li,Qian ZhiHan,et al. The application of the instantaneous states reduction to the orbital monitoring of pivotal arcs of the Chang'E-1 satellite[J]. SCIENCE IN CHINA SERIES G-PHYSICS MECHANICS & ASTRONOMY,2009,52(12):1833-1841.
APA Li JinLing,Guo Li,Qian ZhiHan,&Ping JinSong.(2009).The application of the instantaneous states reduction to the orbital monitoring of pivotal arcs of the Chang'E-1 satellite.SCIENCE IN CHINA SERIES G-PHYSICS MECHANICS & ASTRONOMY,52(12),1833-1841.
MLA Li JinLing,et al."The application of the instantaneous states reduction to the orbital monitoring of pivotal arcs of the Chang'E-1 satellite".SCIENCE IN CHINA SERIES G-PHYSICS MECHANICS & ASTRONOMY 52.12(2009):1833-1841.

入库方式: OAI收割

来源:上海天文台

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