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The paper contains original developments for a novel Model Predictive Control (MPC) approach that implements a path-based strategy to perform a safe docking to a tumbling object in LEO. The contribution is instrumental for eventual active debris removal missions by using Cubesats or other small satellites.

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This page is a summary of: Collision-Avoiding Model Predictive Rendezvous Strategy to Tumbling Launcher Stages, Journal of Guidance Control and Dynamics, June 2023, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.g006804.
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