中国科学院机构知识库网格
Chinese Academy of Sciences Institutional Repositories Grid
Problem of algorithm in precision orbit determination

文献类型:期刊论文

作者Liu, L; Zhang, Q; Liao, XH
刊名SCIENCE IN CHINA SERIES A-MATHEMATICS PHYSICS ASTRONOMY
出版日期1999-05-01
卷号42期号:5页码:552-560
关键词orbit determination precision ephemeris state transition matrix analytical method
英文摘要In orbit determination, the precision ephemeris and state transition matrix are usually obtained by solving two groups of ordinary differential equations with numerical integration method due to the complexity of the force models. A kind of simplified analytical method to compute the state transition matrix is given. The method is not only very efficient for the case where the orbit are is not too long, but also can avoid the integration of two groups of ordinary differential equations at the same time. Some practical test examples also show the efficiency of the method.
WOS标题词Science & Technology ; Physical Sciences
类目[WOS]Mathematics, Applied ; Mathematics
研究领域[WOS]Mathematics
收录类别SCI
语种英语
WOS记录号WOS:000081220100013
源URL[http://119.78.226.72/handle/331011/28158]  
专题上海天文台_天文地球动力学研究中心
作者单位1.Nanjing Univ, Dept Astron, Nanjing 210093, Peoples R China
2.Chinese Acad Sci, Shanghai Observ, Shanghai 200030, Peoples R China
推荐引用方式
GB/T 7714
Liu, L,Zhang, Q,Liao, XH. Problem of algorithm in precision orbit determination[J]. SCIENCE IN CHINA SERIES A-MATHEMATICS PHYSICS ASTRONOMY,1999,42(5):552-560.
APA Liu, L,Zhang, Q,&Liao, XH.(1999).Problem of algorithm in precision orbit determination.SCIENCE IN CHINA SERIES A-MATHEMATICS PHYSICS ASTRONOMY,42(5),552-560.
MLA Liu, L,et al."Problem of algorithm in precision orbit determination".SCIENCE IN CHINA SERIES A-MATHEMATICS PHYSICS ASTRONOMY 42.5(1999):552-560.

入库方式: OAI收割

来源:上海天文台

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