Expansion of the perturbing function of a satellite restricted four-body problem

DOI10.1007/BF01229556zbMath0473.70023OpenAlexW2044641940MaRDI QIDQ3928307

V. V. Anikovskij, Sergei Georgievich Zhuravlev

Publication date: 1981

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

Full work available at URL: https://doi.org/10.1007/bf01229556

zbMATH Keywords

artificial satelliteaccuracy of 19th ordereccentricities of orbitsexpansion perturbing functioninclination of the orbitstwo perturbing bodies

Mathematics Subject Classification ID

Astronomy and astrophysics (85A99) Celestial mechanics (70F15) Orbital mechanics (70M20) (n)-body problems (70F10)

Cites Work

• Conditionally periodic solutions of the canonical systems of differential equations in non-autonomous resonant case

This page was built for publication: Expansion of the perturbing function of a satellite restricted four-body problem