Fuel optimization for low-thrust Earth-Moon transfer via indirect optimal control

DOI10.1007/S10569-017-9808-2zbMath1390.70024OpenAlexW2794328213MaRDI QIDQ1640685

Daniel Pérez-Palau, Richard Epenoy

Publication date: 14 June 2018

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

Full work available at URL: https://doi.org/10.1007/s10569-017-9808-2

zbMATH Keywords

low-thrust propulsionbicircular restricted four-body problemEarth-Moon transfersindirect optimal controlminimum-fuel trajectories

Mathematics Subject Classification ID

Numerical optimization and variational techniques (65K10) Numerical methods based on necessary conditions (49M05) (n)-body problems (70F10)

Related Items (1)

Long-term capture orbits for low-energy space missions

Cites Work

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• Survey of Numerical Methods for Trajectory Optimization
• New smoothing techniques for solving bang–bang optimal control problems—numerical results and statistical interpretation
• Low energy transfer to the Moon

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