First order semianalytic satellite theory with recovery of the short period terms due to third body and zonal perturbations

DOI10.1016/0094-5765(81)90108-9zbMath0475.70028OpenAlexW2001676803MaRDI QIDQ3930700

Bernard Kaufman

Publication date: 1981

Published in: Acta Astronautica (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0094-5765(81)90108-9

zbMATH Keywords

large time stepsLie seriesaveraging over eccentric anomalyperturbations due to sun, moon and zonal harmonics of earth

Mathematics Subject Classification ID

Orbital mechanics (70M20) Numerical integration (65D30)

Related Items (2)

Nonsingular vectorial reformulation of the short-period corrections in Kozai's oblateness solution ⋮ Construction of a consistent semianalytic theory of a planetary or moon orbiter perturbed by a third body

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