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 script to have an initial assessment of the spacecraft magnetorquers flight dynamics
🛰️ Detumbling-Simulator is 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. A related paper details the method and simulation results.
Application of kynodynamical motion planning algorithms to perform attitude maneuvers for a magnetorquer-actuated LEO satellite with pointing constrains.
Project Monarch - senior design project
Remote Control from ground Cubesat
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