On optimal three-impulse Earth-Moon transfers in a four-body model

DOI10.1007/S10569-024-10193-4zbMATH Open1547.70022MaRDI QIDQ6573419

Carmine Giordano, Carmine Buonagura, Francesco Topputo, Guido Grossi

Publication date: 16 July 2024

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

zbMATH Keywords

primer vector theoryfuel-optimal trajectorythree-impulse transfer

Mathematics Subject Classification ID

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

Cites Work

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• Optimal control with aerospace applications
• A study of low-energy transfer orbits to the Moon: towards an operational optimization technique
• Sun-perturbed Earth-to-Moon transfers with low energy and moderate flight time
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• Low-energy transfers to the Moon with long transfer time
• Primer vector on fixed-time impulsive trajectories.
• An efficient method for calculating optimal free-space n-impulse trajectories.
• On the dynamics of weak stability boundary lunar transfers

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