ADCS_sim_cubesat

Simulate and visualize a CubeSat’s attitude dynamics using Earth’s magnetic field and on-board magnetic torquers.
This SCILAB-based framework computes quaternion evolution, angular rates, pointing error, magnetic dipole moments, and applied control torques.

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🚀 Features

• Quaternion Dynamics: Full 3-axis kinematic propagation.
• Magnetic Torquer Control: Bang-bang and PD controllers using Earth’s magnetic field model.
• Performance Metrics: Settling time, steady-state pointing error, mean & peak dipole moment.
• Automated Logging: Save simulation outputs and plotted figures.

Contact Information

For questions or support, contact Team SRMSAT at [[email protected]].