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A trajectory design procedure for a low-thrust enabled small satellite is presented. This procedure is used to design a trajectory for a SmallSat and a CubeSat to the Sun-Earth L5 region from a near-Earth deployment condition.
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This page is a summary of: Designing Low-Thrust Trajectories for a SmallSat Mission to Sun–Earth L5, Journal of Guidance Control and Dynamics, October 2020, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.g004993.
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