Analytical methods for the orbits of artificial satellites of the Moon

DOI10.1007/BF01228033zbMath0218.70014OpenAlexW2057302585MaRDI QIDQ5623265

N. G. Kochina, L. S. Evdokimova, V. A. Brumberg

Publication date: 1971

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

Full work available at URL: https://doi.org/10.1007/bf01228033

Mathematics Subject Classification ID

Orbital mechanics (70M20)

Related Items (5)

Analytical linear perturbation theory for highly eccentric satellite orbits ⋮ Derivative of Kaula's inclination function ⋮ A resonant-term-based model including a nascent disk, precession, and oblateness: application to GJ 876 ⋮ Long-term evolution of orbits about a precessing oblate planet: III: A semianalytical and a purely numerical approach ⋮ Long-term evolution of orbits about a precessing oblate planet. I: The case of uniform precession

Cites Work

• The motion of a lunar satellite
• A semi-analytic theory for the motion of a lunar satellite
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