Solution set on the natural satellite formation orbits under first-order Earth's non-spherical perturbation

DOI10.1007/s10409-005-0063-5zbMath1200.70031OpenAlexW1987369974MaRDI QIDQ608662

Humei Wang, Jun-Feng Li, Wei Yang

Publication date: 25 November 2010

Published in: Acta Mechanica Sinica (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s10409-005-0063-5

zbMATH Keywords

perturbationorbital mechanicsorbital elementsreference orbital elementssatellite formation flight

Mathematics Subject Classification ID

Orbital mechanics (70M20)

Related Items (1)

Approximate analysis for relative motion of satellite formation flying in elliptical orbits

Cites Work

• Dynamical behaviors and relative trajectories of the spacecraft formation flying
• \(J_2\) invariant relative orbits for spacecraft formations

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