ADCS simulations for the AcubeSAT nanosatellite
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Updated
Jul 3, 2024 - MATLAB
ADCS simulations for the AcubeSAT nanosatellite
Implementations of the major developments in 3D-attitude determination of spacecraft including the Triad method and various solutions to the Wahba's problem.
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 simplified MATLAB simulator for magnetic detumbling of fast-tumbling picosatellites.
Simple J2 propagator modeled in Simulink
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