Effect of oblateness of an artificial satellite on the orbits around the triangular points of the Earth-Moon system in the axisymmetric ER3BP
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Publication:513381
DOI10.1007/S12591-014-0232-8zbMath1393.70040OpenAlexW2050682760MaRDI QIDQ513381
Publication date: 6 March 2017
Published in: Differential Equations and Dynamical Systems (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1007/s12591-014-0232-8
periodic orbitsMoonEarthtriangular pointscelestial mechanicselliptic restricted three-body problem (ER3BP)
Related Items (4)
A study of periodic orbits near Europa ⋮ Collinear points in the photogravitational ER3BP with zonal harmonics of the secondary ⋮ The effect of zonal harmonics on dynamical structures in the circular restricted three-body problem near the secondary body ⋮ The effect of perturbations on the circular restricted four-body problem with variable masses
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