Lie-series for orbital elements. I: The planar case

DOI10.1007/s10569-014-9548-5zbMath1294.70009arXiv1403.7901OpenAlexW2021142394MaRDI QIDQ740357

András Pál

Publication date: 2 September 2014

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

Full work available at URL: https://arxiv.org/abs/1403.7901

zbMATH Keywords

numerical methodsrecurrence relationsTaylor coefficientsLie-integrationplanetary systems\(N\)-body problems

Mathematics Subject Classification ID

Celestial mechanics (70F15) Galactic and stellar dynamics (85A05) (n)-body problems (70F10) Numerical integration (65D30) Approximation methods and numerical treatment of dynamical systems (37M99)

Related Items (1)

Lie-series for orbital elements. II: The spatial case

Cites Work

• Numerical integration of dynamical systems with Lie series
• A new set of integrals of motion to propagate the perturbed two-body problem
• Integration of the elliptic restricted three-body problem with Lie series
• Unnamed Item
• Unnamed Item
• Unnamed Item

This page was built for publication: Lie-series for orbital elements. I: The planar case