Canonical elements and Keplerian-like solutions for intermediary orbits of satellites of an oblate planet

DOI10.1007/BF00692474zbMath0819.70009OpenAlexW1628592035MaRDI QIDQ1311634

Luis Mario Floría

Publication date: 21 January 1994

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

Full work available at URL: https://doi.org/10.1007/bf00692474

zbMATH Keywords

analytical solutionHamilton-Jacobi equationextended phase spaceelementary functionsgeneral Hamiltonianmajor secular effects

Mathematics Subject Classification ID

Two-body problems (70F05) Celestial mechanics (70F15) Orbital mechanics (70M20)

Cites Work

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• Mechanics. From Newton's laws to the deterministic chaos.
• An analytic solution for theJ 2 perturbed equatorial orbit
• Elimination of the perigee in the satellite problem
• On the radial intermediaries and the time transformation in satellite theory
• The elimination of the parallax in satellite theory
• The extended phase space formulation of the Vinti problem

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