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We propose a novel three-level framework to optimize the trajectory of multiple spacecraft rendezvous missions in low earth orbits. It was tested by the problem of 9th global trajectory optimization competition and better solution was found.
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This page is a summary of: Global Optimization of Multiple-Spacecraft Rendezvous Mission via Decomposition and Dynamics-Guide Evolution Approach, Journal of Guidance Control and Dynamics, January 2022, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.g006101.
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