Analytical linear perturbation theory for highly eccentric satellite orbits

DOI10.1007/BF00049516zbMath0829.70008MaRDI QIDQ1898002

Thomas Konrad, Eugene Brumberg, Michael H. Soffel, V. A. Brumberg

Publication date: 25 January 1996

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

zbMATH Keywords

elliptic anomalyelliptic function expansionsKaula's theory

Mathematics Subject Classification ID

Celestial mechanics (70F15) Orbital mechanics (70M20)

Related Items (3)

Dynamics of highly eccentric and highly inclined space debris ⋮ Exploring the long-term dynamics of perturbed Keplerian motion in high degree potential fields ⋮ Parameterized post-Newtonian orbital effects in extrasolar planets

Cites Work

• Computation of elliptic Hansen coefficients and their derivatives
• Expansions of elliptic motion based on elliptic function theory
• Note on Lagrange's inversion formula
• Analytical methods for the orbits of artificial satellites of the Moon
• Unnamed Item
• Unnamed Item
• Unnamed Item

This page was built for publication: Analytical linear perturbation theory for highly eccentric satellite orbits