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By introducing three assumptions in combination with an initial guess technique, this paper presents an efficient indirect trajectory optimization method to solve the low-thrust many-revolution transfers within the planetary system.
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This page is a summary of: Low-Thrust Trajectory Optimization with Averaged Dynamics Using Analytical Switching Detection, Journal of Guidance Control and Dynamics, June 2024, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.g007858.
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