An optimum method for calculating restricted three-body orbits

IF 1.6 3区物理与天体物理 Q3 ASTRONOMY & ASTROPHYSICS

Celestial Mechanics & Dynamical Astronomy Pub Date : 1988-03-01 DOI:10.1007/BF01228999

M. Murison

引用次数: 1

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计算受限三体轨道的最佳方法

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来源期刊

Celestial Mechanics & Dynamical Astronomy 地学天文-数学跨学科应用

CiteScore

3.00

自引率

12.50%

发文量

审稿时长

6 months

期刊介绍： The international journal Celestial Mechanics and Dynamical Astronomy is concerned with the broad topic of celestial mechanics and its applications, as well as with peripheral fields. The papers published in Celestial Mechanics and Dynamical Astronomy include treatments of the mathematical, physical and computational aspects of planetary theory, lunar theory, general and special perturbation theory, ephemerides, resonance theory, geodesy of the Earth and the planets, dynamics, the 3-body problem, the n-body problem, space mechanics, ring systems, galactic dynamics, reference frames, time, relativity, nongravitational forces, computer methods, computer languages for analytical developments, and database management. Celestial Mechanics and Dynamical Astronomy is the journal of record in its field and is an indispensable component of reference libraries on Dynamical Astronomy, Astrodynamics and Dynamical Systems.