Ejection-collision orbits with the more massive primary in the planar elliptic restricted three body problem

DOI10.1007/BF00049513zbMath0830.70007OpenAlexW2093657054MaRDI QIDQ1897999

Conxita Pinyol

Publication date: 20 September 1995

Published in: Celestial Mechanics and Dynamical Astronomy (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/bf00049513

zbMATH Keywords

approximation to initial conditionsperturbation of two-body problemregularization of variables

Mathematics Subject Classification ID

Three-body problems (70F07)

Related Items (9)

Pulsating different curves of zero velocity around triangular equilibrium points in elliptical restricted three-body problem ⋮ Regularization of the Hill four-body problem with oblate bodies ⋮ Computer assisted proofs for transverse collision and near collision orbits in the restricted three body problem ⋮ To and fro motion for the hydrogen atom in a circularly polarized microwave field ⋮ Ejection-collision orbits in the RTBP ⋮ Regularisation in Ejection-Collision Orbits of the RTBP ⋮ Analytical and numerical results on families of \(n\)-ejection-collision orbits in the RTBP ⋮ Transit regions and ejection/collision orbits in the RTBP ⋮ Non-linear stability of triangular equilibrium points in ER3BP under radiating primaries in presence of resonance

Cites Work

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• Triple collision in the collinear three-body problem
• Collision orbits in the anisotropic Kepler problem
• Parabolic orbits in the elliptic restricted three-body problem
• On the elliptic restricted three-body problem
• Oscillatory solutions in the planar restricted three-body problem
• A note on the existence of invariant punctured tori in the planar circular restricted three-body problem
• Stability of planetary orbits in binary systems

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