Efficient design of direct low-energy transfers in multi-moon systems

Title
Efficient design of direct low-energy transfers in multi-moon systems
Authors
Keywords
Spacecraft trajectories, Low-energy transfers, Circular restricted three-body problem, Restricted two-body problem, Galilean moons
Journal
CELESTIAL MECHANICS & DYNAMICAL ASTRONOMY
Volume 127, Issue 4, Pages 429-450
Publisher
Springer Nature
Online
2016-10-18
DOI
10.1007/s10569-016-9733-9

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