An approximate integral and solution for eccentric planetary type orbits in the restricted problem of three bodies

DOI10.1007/BF00048765zbMath0745.70005OpenAlexW2035208658MaRDI QIDQ1186218

S. Singh

Publication date: 28 June 1992

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

Full work available at URL: https://doi.org/10.1007/bf00048765

zbMATH Keywords

perturbation theoryangular momentumrenormalization transformationasymptotic Fourier methodquasi-integral of motionsecond integral

Mathematics Subject Classification ID

Three-body problems (70F07) Celestial mechanics (70F15)

Uses Software

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Cites Work

• Numerical experiments on planetary orbits in double stars
• An analytical study of stable planetary orbits in the circular restricted problem
• Integration theory for the restricted three-body-problem with application to P-type orbits
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