6DOF simulation of a CubeSat detumbling in LEO under 3-axis magnetic control using a B-dot controller and LPFs in closed-loop feedback.
🛰️ MATLAB simulator for pure magnetic detumbling of fast-tumbling picosatellites: B-dot control, IGRF environment, realistic magnetorquers and magnetometers, and Monte Carlo campaigns. Code behind the IAC-18 paper.
DDPG-based robotic trajectory planning for space debris detumbling using eddy currents and a 6-DOF manipulator.
Project Monarch - senior design project
Simulink simulation of a spacecraft dynamics to develop closed-loop attitude control algorithms with constant thrust jets, magnetometer, star and Sun sensor
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