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Capturing an asteroid requires using a lot of fuel, which in turn makes such a space mission very costly. This paper proposes a novel trajectory design to minimize such costs, by using a framework of increasingly higher accuracy models of motion to move asteroids to a near-Earth orbit.

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This page is a summary of: Multifidelity Design of Low-Thrust Resonant Captures for Near-Earth Asteroids, Journal of Guidance Control and Dynamics, February 2019, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.g003599.
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