The post-Newtonian effects in the critical inclination problem in artificial satellite theory

DOI10.1016/j.amc.2003.12.041zbMath1122.70021OpenAlexW2035481340MaRDI QIDQ1764736

Xianqiang Yang

Publication date: 22 February 2005

Published in: Applied Mathematics and Computation (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.amc.2003.12.041

zbMATH Keywords

Hamiltonian perturbationsCritical inclinationpost-Newtonian

Mathematics Subject Classification ID

Celestial mechanics (70F15) Orbital mechanics (70M20)

Related Items (2)

Invariant relative orbits for satellite constellations: a second-order theory ⋮ Canonical solution of the critical inclination problem taking into account PN-corrections

Uses Software

• MACSYMA

Cites Work

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• Relativistic effects in the motion of artificial satellites: The oblateness of the central body. II
• Relativistic effects in the critical inclination problem in artificial satellite theory
• Analytical solutions to the four post-Newtonian effects in a near-Earth satellite orbit
• The ?critical inclination?: Another look
• Expansion formulae in canonical transformations depending on a small parameter

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