Motion of artificial satellites in the set of Eulerian redundant parameters. III

DOI10.1007/BF00056354zbMath0850.70279OpenAlexW3008699493MaRDI QIDQ1185074

Samiha Al-Sayed Abdullah Najmuldeen, Mervat El-Sayed Awad, Mohamed Abel Sharaf

Publication date: 28 June 1992

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

Full work available at URL: https://doi.org/10.1007/bf00056354

Mathematics Subject Classification ID

Orbital mechanics (70M20)

Related Items (5)

A new set of integrals of motion to propagate the perturbed two-body problem ⋮ A special perturbation method in orbital dynamics ⋮ Analytical solution to the perturbed \(J_ 2\) motion of artificial satellite in terms of Euler parameters ⋮ Note on the ideal frame formulation ⋮ DROMO propagator revisited

Cites Work

• Unnamed Item
• The motion of artificial satellites in the set of Eulerian redundant parameters
• Orbits near critical inclination, including lunisolar perturbations
• Time elements in rectangular coordinates
• The intermediate anomaly
• Keplerian motion and gyration

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