Minimum fuel trajectories for round trip lunar missions

DOI10.1007/s40314-017-0533-yzbMath1446.70045OpenAlexW2769330056MaRDI QIDQ1993639

Luiz Arthur Gagg Filho, Sandro da Silva Fernandes

Publication date: 5 November 2018

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

Full work available at URL: https://doi.org/10.1007/s40314-017-0533-y

zbMATH Keywords

three-body problemfour-body problemoptimal Earth-Moon trajectoriespatched-conic approximationround trip lunar missions

Mathematics Subject Classification ID

Applications of optimal control and differential games (49N90) Orbital mechanics (70M20)

Cites Work

• Unnamed Item
• Unnamed Item
• Unnamed Item
• Unnamed Item
• Optimal round trip lunar missions based on the patched-conic approximation
• Shooting and numerical continuation methods for computing time-minimal and energy-minimal trajectories in the Earth-Moon system using low propulsion
• Primal-dual properties of sequential gradient-restoration algorithms for optimal control problems. II: General problem
• Sun-perturbed Earth-to-Moon transfers with low energy and moderate flight time
• Modifications and extensions of the sequential gradient-restoration algorithm for optimal control theory
• 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

This page was built for publication: Minimum fuel trajectories for round trip lunar missions