Implementations of the major developments in 3D-attitude determination of spacecraft including the Triad method and various solutions to the Wahba's problem.
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Updated
Dec 26, 2023 - MATLAB
Implementations of the major developments in 3D-attitude determination of spacecraft including the Triad method and various solutions to the Wahba's problem.
ADCS simulations for the AcubeSAT nanosatellite
6DOF simulation of a CubeSat detumbling in LEO under 3-axis magnetic control using a B-dot controller and LPFs in closed-loop feedback.
Simple J2 propagator modeled in Simulink
A simplified MATLAB simulator for magnetic detumbling of fast-tumbling picosatellites.
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