The equations of motion of the joint effects of the relativistic and solar radiation pressure on an Earth artificial satellite.

DOI10.1016/S0096-3003(03)00144-9zbMath1100.70017MaRDI QIDQ1427871

A. A. El-Enna

Publication date: 14 March 2004

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

Mathematics Subject Classification ID

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

Related Items (1)

Analytical treatment of the relativistic and solar radiation pressure effects on an artificial satellite

Cites Work

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• Relativistic effects for near-Earth satellite orbit determination
• 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 effect of direct solar radiation pressure on a spacecraft of complex shape. I: The equations of motion. II: The solutions
• Some special orbits in the two-body problem with radiation pressure
• Orbital perturbations due to radiation pressure for a spacecraft of complex shape
• Canonical transformations depending on a small parameter

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