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jgg
2007 27 (1):
85-90
ISSN: 0412-1961 CN: 21-1139/TG
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LEO SATELLITE EPHEMERIS PARAMETERS FITTING METHOD BASED ON ORBIT CHARACTER OF SATELLITE |
Ma Kaifeng 1,2) ; Peng Bibo 1) ; and Hong Ying 3) |
1)Institute of Geodesy and Geophysics,CAS,Wuhan 4300772)Graduate School of the Chinese Academy of Science,Beijing 1000493)Department of Math. and Physics,Wuhan University of Science and Engineering,Wuhan 430073 |
Received: 1900-01-01 Revised: 1900-01-01 Online: null |
Supporting info null |
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