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

DOI10.1016/S0096-3003(02)00108-XzbMath1023.70013OpenAlexW2048829941MaRDI QIDQ1406138

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

Publication date: 9 September 2003

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

Full work available at URL: https://doi.org/10.1016/s0096-3003(02)00108-x

zbMATH Keywords

small parametercanonical transformationphase spacesolar radiation pressureDelaunay elementsEarth oblatenesspost-Newtonian potentialsecond zonal harmonic

Mathematics Subject Classification ID

Celestial mechanics (70F15) Orbital mechanics (70M20) Waves and radiation in optics and electromagnetic theory (78A40)

Cites Work

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• Relativistic effects in the motion of artificial satellites: The oblateness of the central body. II
• The relativistic and direct solar radiation pressure effects on an axially symmetric spacecraft. I: The Hamiltonian and the canonical equations of motion.
• Two-body motion in the post-Newtonian approximation
• Expansion formulae in canonical transformations depending on a small parameter

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