Physics
Scientific paper
May 1979
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1979kosis..17..333m&link_type=abstract
Kosmicheskie Issledovaniia, vol. 17, May-June 1979, p. 333-341. In Russian.
Physics
1
Gravitational Effects, Libration, Orbital Mechanics, Satellite Rotation, Three Body Problem, Differential Equations, Earth-Moon System, Euler Equations Of Motion, Resonance
Scientific paper
The paper considers the motion of a satellite relative to its center of mass near a collinear libration point L2 in the restricted circular three body problem. The satellite is considered to be a rigid body whose center of mass moves on a periodic orbit near L2 in the rotation plane of the principal attractive masses. Emphasis is placed on two-dimensional motion, for which one of the principal central axes of inertia of the satellite is normal to the orbit plane during the entire course of the motion. Periodic motions are obtained and their stability is investigated on the assumption that the ellipsoid of inertia of the satellite deviates negligibly from an ellipsoid of revolution.
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