A Method to Design Efficient Low-Energy, Low-Thrust Transfers to the Moon

DOI10.1007/978-1-4614-0231-2_2zbMath1229.37113OpenAlexW1556291225MaRDI QIDQ3112514

G. Mingotti, Francesco Topputo, Franco Bernelli-Zazzera

Publication date: 10 January 2012

Published in: Nonlinear and Complex Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/978-1-4614-0231-2_2

Mathematics Subject Classification ID

Dynamical systems in classical and celestial mechanics (37N05) (n)-body problems (70F10)

Related Items (3)

Low-energy transfers to the Moon with long transfer time ⋮ Combined low-thrust propulsion and invariant manifold trajectories to capture NEOs in the Sun-Earth circular restricted three-body problem ⋮ A study of low-energy transfer orbits to the Moon: towards an operational optimization technique

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