Analytical solution to the perturbed \(J_ 2\) motion of artificial satellite in terms of Euler parameters

DOI10.1007/BF00627766zbMath0846.70019OpenAlexW2034128513MaRDI QIDQ1911221

Mervat El-Sayed Awad

Publication date: 5 June 1996

Published in: Earth, Moon, and Planets (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/bf00627766

zbMATH Keywords

oblateness of EarthCayley-Klein type complex variables

Mathematics Subject Classification ID

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

Related Items (2)

A special perturbation method in orbital dynamics ⋮ DROMO propagator revisited

Cites Work

• Unnamed Item
• Motion of artificial satellites in the set of Eulerian redundant parameters. III
• The motion of artificial satellites in the set of Eulerian redundant parameters
• A noncanonical analytic solution to theJ 2 perturbed two-body problem
• Orbits near critical inclination, including lunisolar perturbations
• The gravity-perturbed Lambert problem: A KS variation of parameters approach
• An analytic solution to the classical two-body problem with drag

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