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,Orbit Determination with the Keplerian Integrals,mal property of this polynomial is proved using Gröbner bases theory. The second method (.) is thought for the linkage of 3 TSAs, and leads to a univariate polynomial equation of degree 8. A numerical test is shown for both algorithms.大厅 发表于 2025-3-27 17:25:59
2194-1009 of results both concerning the theory and the effective impl.This volume contains the detailed text of the major lectures delivered during the I-CELMECH Training School 2020 held in Milan (Italy). The school aimed to present a contemporary review of recent results in the field of celestial mechanics现存 发表于 2025-3-27 17:47:28
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978-3-031-13117-2The Editor(s) (if applicable) and The Author(s), under exclusive license to Springer Nature SwitzerlAtmosphere 发表于 2025-3-28 02:39:46
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