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Orbit insertion at Saturn requires a large manoeuver with chemical thrusters to compensate for the velocity difference between the spacecraft and the planet. We present a low-thrust control law to reduce substantially the velocity relative to Saturn on arrival, thus facilitating the capture of the spacecraft.
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This page is a summary of: Reduction of Saturn Orbit Insertion Impulse Using Deep-Space Low Thrust, Journal of Guidance Control and Dynamics, April 2020, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.g004587.
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