Shooting and numerical continuation methods for computing time-minimal and energy-minimal trajectories in the Earth-Moon system using low propulsion

DOI10.3934/dcdsb.2012.17.245zbMath1235.49051OpenAlexW2332702047MaRDI QIDQ765005

Gautier Picot

Publication date: 19 March 2012

Published in: Discrete and Continuous Dynamical Systems. Series B (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.3934/dcdsb.2012.17.245

zbMATH Keywords

geometric control theory3-body problemenergy minimization problemEarth-Moon transfernumerical analysis methodtime minimization problem

Mathematics Subject Classification ID

Numerical methods based on necessary conditions (49M05) Three-body problems (70F07) Optimality conditions for problems involving ordinary differential equations (49K15)

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