Titlebook: Dynamical Trapping and Evolution in the Solar System; Proceedings of the 7 Vassilis V. Markellos,Yoshihide Kozai Conference proceedings 198

forebear

Orientation of a Satellite Located at the Libration Point in the Restricted Three-Body Problemy problem are given. This problem was analyzed in part by Kane and Marsh (1971), Markeev (1967a,b). However the present investigation is formulated in terms of hamiltonian mechanics. The final results will by used to study nonlinear effects connected with the gravitational influence of the “second”

OGLE

Theory of the Libration of the Moonld. This field is represented through its fourth degree harmonics for the torque due to the Earth (the second degree for the torque due to the Sun). The Moon is assumed to be rigid and its orbital motion is described by the ELP 2000 solution (Chapront and Chapront-Touzé 1981) for the main problem of

擴(kuò)大

Formidable

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