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引用本文:马开锋,彭碧波,洪樱. �������ǹ�������ĵ͹���������������Ϸ�[J]. 大地测量与地球动力学, 2007, 27(1): 85-90
作者姓名:马开锋  彭碧波  洪樱
作者单位:1. 中国科学院测量与地球物理研究所,武汉,430077;中国科学院研究生院,北京,100049
2. 中国科学院测量与地球物理研究所,武汉,430077
3. 武汉科技学院数理系,武汉,430073
基金项目:国家自然科学基金(40234039)
摘    要:???????????????仯????????????????GPS??????????????????????????????????????????????????????????????????????λ?ü????????????????????????????????????GPS??????15????????????25????????????????????????????????????25??????????????????????????????

关 键 词:GPS??????  ???????  ???????  ????????  ??????  
文章编号:1671-5942(2007)01-0085-06
修稿时间:2006-07-14

LEO SATELLITE EPHEMERIS PARAMETERS FITTING METHOD BASED ON ORBIT CHARACTER OF SATELLITE
Ma Kaifeng,Peng Bibo,Hong Ying. LEO SATELLITE EPHEMERIS PARAMETERS FITTING METHOD BASED ON ORBIT CHARACTER OF SATELLITE[J]. Journal of Geodesy and Geodynamics, 2007, 27(1): 85-90
Authors:Ma Kaifeng  Peng Bibo  Hong Ying
Affiliation: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
Abstract:On the basis of the orbit character of the LEO satellite and the advantages of definite physical meanings, quickly creating, high precision, fewer parameters of GPS broadcast ephemeris, a new sort of ephemeris parameters for calculating LEO satellite location is designed and analyzed through a example. Some significant comparisons are made between the 15-parameter method of GPS broadcast ephemeris and the designed 25-parameter method, the results show that the designed 25 parameters method has a higher precision for LEO satellite orbit fitting under the same condition.
Keywords:GPS broadcast ephemeris   LEO satellite   orbit analysis   ephemeris parameter  fitting precision
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