Optimal two-impulse trajectories with moderate flight time for Earth-Moon missions

DOI10.1155/2012/971983zbMath1264.70056OpenAlexW2064529553WikidataQ58912785 ScholiaQ58912785MaRDI QIDQ1955429

Cleverson Maranhão Porto Marinho, Sandro da Silva Fernandes

Publication date: 11 June 2013

Published in: Mathematical Problems in Engineering (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1155/2012/971983

Mathematics Subject Classification ID

Applications of optimal control and differential games (49N90) Three-body problems (70F07) Control of mechanical systems (70Q05) Orbital mechanics (70M20)

Related Items (7)

Optimal round trip lunar missions based on the patched-conic approximation ⋮ Energy analysis of the single impulsive Earth-Moon transfer with the temporary lunar capture ⋮ Searching for orbits with minimum fuel consumption for station-keeping maneuvers: an application to lunisolar perturbations ⋮ Station keeping of constellations using multiobjective strategies ⋮ Minimum fuel trajectories for round trip lunar missions ⋮ Application of a genetic algorithm in orbital maneuvers ⋮ A study of Earth-Moon trajectories based on analytical expressions for the velocity increments

Cites Work

• Sun-perturbed Earth-to-Moon transfers with low energy and moderate flight time
• Computation of low energy Earth-to-Moon transfers with moderate flight time
• Sequential gradient-restoration algorithm for the minimization of constrained functions. Ordinary and conjugate gradient versions
• BURRAU'S PROBLEM OF THREE BODIES
• Low energy transfer to the Moon
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