An implementation of the logarithmic Hamiltonian method for artificial satellite orbit determination

DOI10.1023/A:1015248411856zbMath1088.70004MaRDI QIDQ1610309

Yoshi Hashida, Seppo Mikkola, Phil Palmer

Publication date: 19 August 2002

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

zbMATH Keywords

symplectic integrationstate-transition matrixtwo-body leapfrog

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)

This page was built for publication: An implementation of the logarithmic Hamiltonian method for artificial satellite orbit determination