Construction of a consistent semianalytic theory of a planetary or moon orbiter perturbed by a third body

DOI10.1007/BF01230668zbMath0518.70010MaRDI QIDQ3667984

Ernst Roth

Publication date: 1982

Published in: Celestial Mechanics (Search for Journal in Brave)

zbMATH Keywords

successive approximationsarbitrary ordereccentric anomalyorbiter perturbed by third bodysmall parameter by ratio of masses and ratio of semi-major axes

Mathematics Subject Classification ID

Three-body problems (70F07) Astronomy and astrophysics (85A99) Orbital mechanics (70M20)

Related Items (1)

Application of the stroboscopic method to the stellar three-body problem

Cites Work

• On the higher-order stroboscopic method
• First order semianalytic satellite theory with recovery of the short period terms due to third body and zonal perturbations
• Unnamed Item

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