Efficient symplectic integration of satellite orbits

DOI10.1023/A:1008398121638zbMath0948.70003OpenAlexW154409468MaRDI QIDQ1976127

Seppo Mikkola

Publication date: 20 July 2000

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

Full work available at URL: https://doi.org/10.1023/a:1008398121638

zbMATH Keywords

Hamiltonian systemsymplectic integratortime transformationsorbit calculationgeneralized leapfrogperturbed two-body problems

Mathematics Subject Classification ID

Computational methods for problems pertaining to mechanics of particles and systems (70-08) Two-body problems (70F05) Orbital mechanics (70M20)

Related Items (2)

Symplectic integrators with adaptive timestep applied to spinning compact binaries ⋮ Bandlimited implicit Runge-Kutta integration for astrodynamics

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