Problem of algorithm in precision orbit determination
文献类型:期刊论文
作者 | Liu, L![]() |
刊名 | SCIENCE IN CHINA SERIES A-MATHEMATICS PHYSICS ASTRONOMY
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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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