Invariant relative orbits for satellite constellations: a second-order theory

DOI10.1016/j.amc.2006.01.004zbMath1143.70012OpenAlexW2077678983MaRDI QIDQ945334

M. A. Rassem, I. A. El-Tohamy, F. A. Abd El-Salam, W. A. Rahoma, M. K. M. Ahmed

Publication date: 12 September 2008

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

Full work available at URL: https://doi.org/10.1016/j.amc.2006.01.004

zbMATH Keywords

secular driftperturbative effectsDelaunay canonical elements

Mathematics Subject Classification ID

Orbital mechanics (70M20)

Cites Work

• The post-Newtonian effects in the critical inclination problem in artificial satellite theory
• \(J_2\) invariant relative orbits for spacecraft formations
• Formation flying satellites: Control by an astrodynamicist
• Unnamed Item

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