Solution space exploration of low-thrust minimum-time trajectory optimization by combining two homotopies

DOI10.1016/j.automatica.2022.110798OpenAlexW4312055671MaRDI QIDQ2682341

Qian Xiao, Lincheng Li, Jing-Rui Zhang

Publication date: 31 January 2023

Published in: Automatica (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.automatica.2022.110798

zbMATH Keywords

Newton iterative methodindirect optimizationgeostationary orbit transferlongitude-homotopymaximum thrust magnitude continuationthrust-homotopy

Mathematics Subject Classification ID

Computational methods for problems pertaining to mechanics of particles and systems (70-08) Orbital mechanics (70M20)

Cites Work

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• 3D geosynchronous transfer of a satellite: Continuation on the thrust
• Analysis on reachable set for spacecraft relative motion under low-thrust
• Algorithm 956
• Homotopy method for minimum consumption orbit transfer problem
• Survey of Numerical Methods for Trajectory Optimization
• A set modified equinoctial orbit elements
• Introduction to Numerical Continuation Methods
• New smoothing techniques for solving bang–bang optimal control problems—numerical results and statistical interpretation

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