Weak stability boundary trajectories for the deployment of lunar spacecraft constellations

DOI10.1007/s10569-006-9020-2zbMath1219.70065OpenAlexW2092453995MaRDI QIDQ850694

Paolo Teofilatto, Christian Circi

Publication date: 6 November 2006

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

Full work available at URL: https://doi.org/10.1007/s10569-006-9020-2

zbMATH Keywords

lunar constellationRestricted three- and four-body problemweak stability lunar transfer

Mathematics Subject Classification ID

Celestial mechanics (70F15) Orbital mechanics (70M20) (n)-body problems (70F10)

Related Items (6)

Distributed orbit determination and observability analysis for satellite constellations with angles-only measurements ⋮ Energy analysis of the single impulsive Earth-Moon transfer with the temporary lunar capture ⋮ Intersecting invariant manifolds in spatial restricted three-body problems: design and optimization of Earth-to-halo transfers in the Sun-Earth-Moon scenario ⋮ Using space manifold dynamics to deploy a small satellite constellation around the Moon ⋮ Lissajous trajectories for lunar global positioning and communication systems ⋮ Novel spaceways for reaching the Moon: An assessment for exploration

Cites Work

• Sun-perturbed Earth-to-Moon transfers with low energy and moderate flight time
• On the dynamics of weak stability boundary lunar transfers
• Low energy transfer to the Moon
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