Adjoints estimation methods for impulsive Moon-to-Earth trajectories in the restricted three-body problem

DOI10.1002/OCA.2120zbMath1329.49079OpenAlexW1933477049MaRDI QIDQ3459280

Lorenzo Casalino, HongXin Shen, Hai-yang Li

Publication date: 21 December 2015

Published in: Optimal Control Applications and Methods (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1002/oca.2120

zbMATH Keywords

optimal controlhomotopy methodrestricted three-body problemshooting methodindirect methodimpulsive Moon-to-Earth trajectories

Mathematics Subject Classification ID

Newton-type methods (49M15) Applications of optimal control and differential games (49N90) Variable mass, rockets (70P05)

Cites Work

• Continuation from a flat to a round Earth model in the coplanar orbit transfer problem
• Survey of Numerical Methods for Trajectory Optimization
• New smoothing techniques for solving bang–bang optimal control problems—numerical results and statistical interpretation

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