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Missions of active debris removal in low Earth orbits require the use of precise models of the relative dynamics. We propose an analytical framework that uses relative orbital elements as variables and that is also applicable to far-range rendezvous scenarios as well as to large relative orbits.

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This page is a summary of: Analytical Framework for Precise Relative Motion in Low Earth Orbits, Journal of Guidance Control and Dynamics, May 2020, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.g004716.
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