Behaviour of a new type of Runge-Kutta methods when integrating satellite orbits

DOI10.1023/A:1008387322426zbMath0970.70004OpenAlexW1620241354MaRDI QIDQ1568164

Pablo Martín, David J. López, Ana-Belén González

Publication date: 16 October 2001

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

Full work available at URL: https://doi.org/10.1023/a:1008387322426

zbMATH Keywords

numerical integrationlinearizationsymplectic integratorlocal truncation errorperturbed oscillatorssmall perturbation parameterlong-term satellite orbitsRunge-Kutta version of Scheifele \(G\)-function method

Mathematics Subject Classification ID

Computational methods for problems pertaining to mechanics of particles and systems (70-08) Orbital mechanics (70M20) Numerical methods for Hamiltonian systems including symplectic integrators (65P10)

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