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科研机构
上海天文台 [39]
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期刊论文 [33]
学位论文 [6]
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2019 [1]
2018 [1]
2015 [2]
2014 [1]
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2012 [2]
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A new method to determine the gravity field of small bodies from line-of-sight acceleration data
期刊论文
RESEARCH IN ASTRONOMY AND ASTROPHYSICS, 2019, 卷号: 19, 期号: 3, 页码: 10
作者:
Jian, Nian-Chuan
;
Yan, Jian-Guo
;
Ping, Jin-Song
;
Barriot, Jean-Pierre
;
Rodriguez, J. Alexis P.
收藏
  |  
浏览/下载:35/0
  |  
提交时间:2019/05/23
line of sight acceleration
Doppler
celestial mechanics
The precise positioning of lunar farside lander using a four-way lander-orbiter relay tracking mode
期刊论文
ASTROPHYSICS AND SPACE SCIENCE, 2018, 卷号: 363, 期号: 11
作者:
Ye, Mao
;
Li, Fei
;
Yan, Jianguo
;
Barriot, Jean-Pierre
;
Hao, Weifeng
收藏
  |  
浏览/下载:36/0
  |  
提交时间:2019/05/23
Lunar Farside
Lander Positioning
Precise Orbit Determination
Four-way Relay Tracking
Chang'e-4
Orbit improvement for Chang'E-5T lunar returning probe with GNSS technique
期刊论文
ADVANCES IN SPACE RESEARCH, 2015, 卷号: 56, 期号: 11, 页码: 2473-2482
作者:
Fan, Min
;
Hu, XiaoGong
;
Dong, Guangliang
;
Huang, Yong
;
Cao, Jianfeng
收藏
  |  
浏览/下载:62/0
  |  
提交时间:2016/01/14
Chinese lunar exploration program
Global navigation satellite system
Weak signal acquisition and tracking performance
Fusion processing of space- and ground-based data
Accuracy of orbit determination and prediction
Precise orbit determination and rapid orbit recovery supported by time synchronization
期刊论文
ADVANCES IN SPACE RESEARCH, 2015, 卷号: 55, 期号: 12, 页码: 2889-2898
作者:
Guo, Rui
;
Zhou, JianHua
;
Hu, XiaoGong
;
Liu, Li
;
Tang, Bo
收藏
  |  
浏览/下载:29/0
  |  
提交时间:2015/08/07
Time synchronization
Precise orbit determination
Clock offset
Satellite laser ranging
User equivalent range error
Satellite-station time synchronization information based real-time orbit error monitoring and correction of navigation satellite in Beidou System
期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2014, 卷号: 57, 期号: 7, 页码: 1395-1403
作者:
He Feng
;
Zhou ShanShi
;
Hu XiaoGong
;
Zhou JianHua
;
Liu Li
收藏
  |  
浏览/下载:24/0
  |  
提交时间:2015/05/20
satellite navigation
orbital mechanics
time synchronization
ephemeris fitting
Satellite orbit determination combining C-band ranging and differenced ranges by transfer
期刊论文
CHINESE SCIENCE BULLETIN, 2013, 卷号: 58, 期号: 19, 页码: 2323-2328
作者:
Yang Ying
;
Yang XuHai
;
Li ZhiGang
;
Feng ChuGang
收藏
  |  
浏览/下载:17/0
  |  
提交时间:2015/08/03
differenced ranges by transfer
orbital overlapping
orbit prediction
Precise orbit determination of Haiyang-2 using satellite laser ranging
期刊论文
CHINESE SCIENCE BULLETIN, 2013, 卷号: 58, 期号: 6, 页码: 589-597
作者:
Zhao Gang
;
Zhou XuHua
;
Wu Bin
收藏
  |  
浏览/下载:13/0
  |  
提交时间:2014/09/22
Haiyang-2
satellite laser ranging
precise orbit determination
Satellite orbit determination by transfer with differenced ranges
期刊论文
CHINESE SCIENCE BULLETIN, 2012, 卷号: 57, 期号: 36, 页码: 4701-4706
作者:
Yang Ying
;
Li ZhiGang
;
Yang XuHai
;
Feng ChuGang
;
Cao Fen
收藏
  |  
浏览/下载:26/0
  |  
提交时间:2015/08/04
transfer
differenced ranges
precise orbit determination (POD)
orbit prediction
Positioning reduction in the real-time phase of Chang'E-2 satellite
期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2012, 卷号: 55, 期号: 2, 页码: 371-374
作者:
Li JinLing
;
Liu Li
;
Zheng WeiMin
;
Sun ZhongMiao
收藏
  |  
浏览/下载:21/0
  |  
提交时间:2015/08/04
lunar exploration
VLBI
trajectory monitoring
positioning reduction
Chang'E-2 satellite
The Chang'E-1 orbiter plays a distinctive role in China's first successful selenodetic lunar mission
期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2011, 卷号: 54, 期号: 12, 页码: 2130-2144
作者:
Ping JinSong
;
Su XiaoLi
;
Huang Qian
;
Yan JianGuo
收藏
  |  
浏览/下载:12/0
  |  
提交时间:2015/08/19
Chang'E-1
lunar orbiter
lunar science
selenodesy
topography
gravity
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