Optimal round trip lunar missions based on the patched-conic approximation

DOI10.1007/s40314-015-0247-yzbMath1348.70066OpenAlexW624864565MaRDI QIDQ338274

Sandro da Silva Fernandes, Luiz Arthur Gagg Filho

Publication date: 4 November 2016

Published in: Computational and Applied Mathematics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s40314-015-0247-y

zbMATH Keywords

optimal Earth-Moon trajectoriespatched-conic approximationround trip lunar missions

Mathematics Subject Classification ID

Orbital mechanics (70M20)

Related Items (3)

Minimum fuel trajectories for round trip lunar missions ⋮ Interplanetary patched-conic approximation with an intermediary swing-by maneuver with the Moon ⋮ A study of Earth-Moon trajectories based on analytical expressions for the velocity increments

Cites Work

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• Computation of low energy Earth-to-Moon transfers with moderate flight time
• Optimal two-impulse trajectories with moderate flight time for Earth-Moon missions
• Sequential gradient-restoration algorithm for the minimization of constrained functions. Ordinary and conjugate gradient versions
• Sequential gradient-restoration algorithm for optimal control problems
• Optimization of Low-Energy Transfers
• Low energy transfer to the Moon

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