What is it about?
We develop a novel optimization approach to compute the minimum time of low-thrust orbital rendezvous from a fixed initial state to a moving target. With this approach, the best local solution of the minimum-time rendezvous problem can be found easily.
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This page is a summary of: Minimum-Time Rendezvous via Simplified Initial Costate Normalization and Auxiliary Orbital Transfer, Journal of Guidance Control and Dynamics, May 2023, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.g007268.
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