Formulation of the restricted three-body problem with two-center problem orbits as intermediate orbits

DOI10.1007/BF00648654zbMath0472.70006OpenAlexW2045115562MaRDI QIDQ1157930

Ray G. Langebartel

Publication date: 1981

Published in: Astrophysics and Space Science (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/bf00648654

zbMATH Keywords

restrictedearth-moon space travelfigure- eight type orbitstwo-center problem orbits as intermediate orbits

Mathematics Subject Classification ID

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

Cites Work

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• Fourier Expansions of Rational Fractions of Elliptic Integrals and Jacobian Elliptic Functions

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