6DOF simulation of a CubeSat detumbling in LEO under 3-axis magnetic control using a B-dot controller and LPFs in closed-loop feedback.
ADCS simulations for the AcubeSAT nanosatellite
Simple J2 propagator modeled in Simulink
This repository contains the MATLAB simulation and related resources for the paper titled "Non-Linear Control Strategies for Attitude Maneuvers in a CubeSat with Three Reaction Wheels"
🛰️ 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.
Add a description, image, and links to the adcs topic page so that developers can more easily learn about it.
To associate your repository with the adcs topic, visit your repo's landing page and select "manage topics."