The relativistic and direct solar radiation pressure effects on an axially symmetric spacecraft. I: The Hamiltonian and the canonical equations of motion.

DOI10.1016/S0096-3003(01)00208-9zbMath1055.70011MaRDI QIDQ1855854

M. I. El-Saftawy, A. A. El-Enna

Publication date: 28 January 2003

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

zbMATH Keywords

Earth oblatenesspost-Newtonian potential

Mathematics Subject Classification ID

Hamilton's equations (70H05) Celestial mechanics (70F15) Orbital mechanics (70M20) Waves and radiation in optics and electromagnetic theory (78A40)

Related Items (1)

The joint effect of relativistic and direct solar radiation pressure on an axially symmetric spacecraft. II: The solution and the elements of transformation

Cites Work

• Relativistic effects for near-Earth satellite orbit determination
• Analytical solutions to the four post-Newtonian effects in a near-Earth satellite orbit
• Newtonian and relativistic periodic orbits around two fixed black holes
• The effect of direct solar radiation pressure on a spacecraft of complex shape. I: The equations of motion. II: The solutions
• Orbital perturbations due to radiation pressure for a spacecraft of complex shape
• Unnamed Item

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