Third-order secular Solution of the variational equations of motion of a satellite in orbit around a non-spherical planet

DOI10.1007/s10509-012-1038-1zbMath1284.70042OpenAlexW2041747501MaRDI QIDQ2443570

Yanyan Li

Publication date: 8 April 2014

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

Full work available at URL: https://doi.org/10.1007/s10509-012-1038-1

zbMATH Keywords

orbit perturbationsecular variationsEarth oblatenessLagrange equations of motionsatellite Earth orbit

Mathematics Subject Classification ID

Orbital mechanics (70M20) Lagrange's equations (70H03)

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