详细信息   

• 责任者：Yan Jianguo (State Key Laboratory of Information Engineering in Surveying ; Mapping and Remote Sensing ; Wuhan University ; Wuhan 430070 ; China) ; Li Fei
• 刊名：Chinese Journal of Geophysics
• 出版年：2010
• 卷期：53(12)
• 关键词：卫星法 ; satellite methods ; 月球 ; Moon ; 重力场 ; gravity field
• 页码：p.2843-2851
• 图表：4 illus., 4 tables, 24 refs.
• 分类号：0100
• issnNo：ISSN0001-5733
• isbnNo：CN11-2074/P

摘要

The characteristic of Chang’E-1 orbital tracking data is presented in this paper, and the principle and solution strategy of lunar gravity field recovery based on dynamical precise orbit determination are summarized. Under the condition of limited accuracy and coverage of tracking data of Chang’E-1, a lunar gravity field model CEGM-01 up to degree and order 50 is solved independently using six months tracking data. The accuracy of the model CEGM-01 is assessed by multi-means, such as gravity power spectrum, observational residuals after precision orbit determination, lunar surface gravity anomaly character, admittance/coherence with topography model, and the corresponding physical feature and effect are analyzed. The results indicate the effectiveness and reasonability of CEGM-01 solution process. On the basis of current work, the prospect of future development of the gravity field detection is presented in China.