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机构地区:[1]Department of Astronomy and Space Science,Nanjing University,Nanjing 210023,China [2]Institute of Space Environment and Astrodynamics,Nanjing University,Nanjing 210023,China [3]Key Laboratory of Modern Astronomy and Astrophysics,Ministry of Education,Nanjing 210023,China
出 处:《Research in Astronomy and Astrophysics》2024年第5期198-210,共13页天文和天体物理学研究(英文版)
基 金:supported by the National Natural Science Foundation of China(No.12233003);the support from Laboratory of Pinghu,Pinghu,China。
摘 要:Temporary capture efficiency is studied in the framework of the circular restricted three-body problem in two steps.First, a non-uniform distribution of test particles around the secondary's orbit is obtained by fully accounting the secondary's gravitational influence. Second, the capture efficiency is computed based on the non-uniform distribution. Several factors influencing the result are discussed. By studying the capture efficiency in the circular restricted three-body problem of different mass ratios, a power-law relation between the capture efficiency(p) and the mass ratio(μ) is established, which is given by p ≈ 0.27 × μ^(0.53), within the range of 3.0035 ×10^(-6)≤ μ ≤ 3.0034 × 10^(-5). Taking the Sun–Earth system as an example, the influence from the orbit eccentricity of the secondary on the non-uniform distribution and the capture efficiency is studied. Our studies find that the secondary's orbit eccentricity has a negative influence on the capture efficiency.
关 键 词:METHODS numerical-celestial mechanics-planets and satellites dynamical evolution and stability
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