6DOF simulation of a CubeSat detumbling in LEO under 3-axis magnetic control using a B-dot controller and LPFs in closed-loop feedback.
A MATLAB simulator for magnetic detumbling of fast-tumbling picosatellites, featuring a weighted B-dot control algorithm that reduces power consumption while maintaining effective detumbling performance. The repository links to a related paper that outlines the proposed approach and presents simulation results demonstrating its practical benefits.
☄️ Model for contactless space debris detumbling using induced eddy currents with visual simulations.
Project Monarch - senior design project
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