Precise positioning of the Chang’E-3 lunar lander using a kinematic statistical method

Author:

Huang Yong,Hu XiaoGong,Li PeiJia,Cao JianFeng,Jiang DongRong,Zheng WeiMin,Fan Min

Publisher

Springer Science and Business Media LLC

Subject

Multidisciplinary

Reference19 articles.

1. Huang Y. A study on the orbit determination of the Chang’E-1 lunar probe (in Chinese). Ph.D. Thesis. Shanghai: Shanghai Astronomical Observatory, Chinese Academy of Sciences, 2006

2. Chen M, Tang G S, Cao J F, et al. Precision orbit determination of CE-1 lunar satellite. Geomatics Inform Sci Wuhan Univ, 2011, 36: 212–217

3. Li J L, Liu L, Zheng W M, et al. The application of positioning reduction in the realtime stage of the Chang’E-2 project (in Chinese). Sci Sin Phys Mech Astron, 2011, 41: 889–895

4. Liu Q H, Chen M, Xiong W M, et al. Relative position determination of a lunar rover using high-accuracy multi-frequency same-beam VLBI. Sci China Phys Mech Astron, 2010, 53: 571–578

5. Yan J G, Ping J S, Li F, et al. Chang’E-1 precision orbit determination and lunar gravity field solution. Adv Space Res, 2010, 46: 50–57

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