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This work achieves robust attitude tracking of small satellites against parametric uncertainties and persistent disturbances. he performance of the controller is evaluated through numerical simulations and compared with an existing nonlinear algorithm.

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This page is a summary of: Attitude Control of a Small Spacecraft via Tube-Based Model Predictive Control, Journal of Spacecraft and Rockets, November 2019, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.a34394.
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