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Orbit transfers with the use of low thrust include light and eclipse arcs, where propulsion is unavailable. Optimization of these transfers, aimed at minimizing the time of flight, is obtained with two different indirect heuristic approaches.
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This page is a summary of: Optimal Low-Thrust Earth Orbit Transfers with Eclipses Using Indirect Heuristic Approaches, Journal of Guidance Control and Dynamics, February 2024, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.g007797.
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