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《Chinese Journal of Geophysics》 2010-12
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Lunar gravity field model CEGM-01 based on tracking data of Chang'E-1

YAN Jian-Guo~(1,2), LI Fei~1, PING Jin-Song~2, TANG Ge-Shi~3,HUANG Qian~2 , CAO Jian-Feng~(2,3) , LIU Jun-Ze~3 1 State Key Laboratory of Information Engineering in Surveying , Mapping and Remote Sensing ,Wuhan University , Wuhan 430070, China 2 Shanghai Astronomical Observatory , CAS, Shanghai 200030, China 3 Beijing Aerospace Command and Control Center, Beijing 100094, China  
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 our national lunar gravity field detection is presented.
【Fund】: 国家自然科学基金(40904006 40974014 10973031);; 上海市空间导航与定位技术重点实验室开放基金资助
【CateGory Index】: P223
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