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An explicit symplectic integrator for cometary orbits

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Publication:1870198
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DOI10.1023/A:1021125829276zbMath1026.70002OpenAlexW2574257244MaRDI QIDQ1870198

Vyacheslav Emel'yanenko

Publication date: 11 May 2003

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

Full work available at URL: https://doi.org/10.1023/a:1021125829276


zbMATH Keywords

symplectic integrationclose encounterscometary orbithigh eccentricities


Mathematics Subject Classification ID

Computational methods for problems pertaining to mechanics of particles and systems (70-08) Celestial mechanics (70F15) Numerical methods for Hamiltonian systems including symplectic integrators (65P10)


Related Items (2)

A method of symplectic integrations with adaptive time-steps for individual Hamiltonians in the planetary \(N\)-body problem ⋮ A review of structure-preserving numerical methods for engineering applications




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