Low-thrust Lyapunov to Lyapunov and Halo to Halo missions with L2-minimization

DOI10.1051/m2an/2016044zbMath1370.49024arXiv1511.02089OpenAlexW2963058302MaRDI QIDQ5280342

Thomas Haberkorn, Maxime Chupin, Emmanuel Trélat

Publication date: 20 July 2017

Published in: ESAIM: Mathematical Modelling and Numerical Analysis (Search for Journal in Brave)

Full work available at URL: https://arxiv.org/abs/1511.02089

zbMATH Keywords

optimal controlcontinuation methodthree body problemLyapunov orbithalo orbitlow-thrust transferPontryagin's maximum principle (PMP)

Mathematics Subject Classification ID

Numerical methods based on necessary conditions (49M05) Newton-type methods (49M15) Three-body problems (70F07) Control problems involving ordinary differential equations (34H05)

Related Items (2)

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Uses Software

• HOMPACK90
• HamPath

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