Modelling natural formations of LEO satellites

DOI10.1007/S10569-007-9084-7zbMath1162.70328OpenAlexW1971818174MaRDI QIDQ2458482

Yanyan Li

Publication date: 1 November 2007

Published in: Celestial Mechanics and Dynamical Astronomy (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s10569-007-9084-7

zbMATH Keywords

Formation flyingLEORelative motion

Mathematics Subject Classification ID

Orbital mechanics (70M20)

Related Items (4)

Modeling orbital relative motion to enable formation design from application requirements ⋮ Minimum control for spacecraft formations in a J2 perturbed environment ⋮ Collective control of spacecraft swarms for space exploration ⋮ Relative motion of satellites exploiting the super-integrability of Kepler's problem

Cites Work

• Unnamed Item
• The relative motion of earth orbiting satellites
• Satellite relative motion using differential equinoctial elements
• \(J_2\) invariant relative orbits for spacecraft formations

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