Stability of the Moons Orbits in Solar System in the Restricted Three-Body Problem

Ershkov, S.V.

Автор: Ershkov Sergey V.
Журнал: Advances in Astronomy
Том: 2015
Номер: Article number 615029
Год издания: 2015
Первая страница: 1
Последняя страница: 7
DOI: 10.1155/2015/615029
Аннотация: We consider the equations of motion of three-body problem in a Lagrange form (which means a consideration of relative motions of 3-bodies in regard to each other). Analyzing such a system of equations, we consider in details the case of moon’s motion of negligible mass m₃ around the 2-nd of two giant-bodies m₁, m₂ (which are rotating around their common centre of masses on Kepler’s trajectories), the mass of which is assumed to be less than the mass of central body. Under assumptions of R3BP, we obtain the equations of motion which describe the relative mutual motion of the centre of mass of 2-nd giant-body m₂ (Planet) and the centre of mass of 3-rd body (Moon) with additional effective mass placed in that centre of mass. They should be rotating around their common centre of masses on Kepler’s elliptic orbits. For negligible effective mass it gives the equations of motion which should describe a quasi-elliptic orbit of 3-rd body (Moon) around the 2-nd body m₂ (Planet) for most of the moons of the Planets in Solar system. But the orbit of Earth’s Moon should be considered as non-constant elliptic motion for the effective mass 0.0178m₂ placed in the centre of mass for the 3-rd body (Moon). The position of their common centre of masses should obviously differ for the real mass m₃ = 0.0123m₂ and for the effective mass (0.0055+0.0123)m₂ placed in the centre of mass of the Moon.
Добавил в систему: Ершков Сергей Владимирович

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Stability of the Moons Orbits in Solar System in the Restricted Three-Body Problemстатья

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