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Missions of active debris removal in low Earth orbits use forced-motion trajectories during the capture phase. We propose a practical method to compute the piece-wise constant continuous acceleration profile to realize a given guidance plan.
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This page is a summary of: Trajectory Design for Proximity Operations: The Relative Orbital Elements’ Perspective, Journal of Guidance Control and Dynamics, December 2021, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.g006175.
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