机译:Semi-analytical findings for rotational trapped motion of satellite in the vicinity of collinear points {L1, L2} in planar ER3BP
Plekhanov Russian University of Economics||Sternberg Astronomical Institute, M.V. Lomonosov’s Moscow State University;
Odessa State Academy of Civil Engineering and Architecture;
Odessa I. I. Mechnikov National University;
Dynamics of finite-sized satellite; Rotation of finite-sized satellite; Elliptic restricted three-body problem; ER3BP; Trapped motion of satellite; Gravitational potential of MacCullagh type; Quasi-stable elliptic orbit;