Spacecraft Attitude Dynamics and Control

Realtime simulation and control of 3 axis spacecraft with quaternion based control law in presence of external torques. Evaluation of Reaction wheel angular velocity is based on control torques computed using PD controller.

Demo-2 (with charts)

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Area of Interest

Space vehicles, Visualization, Localisation and Mapping, Robots, Position measurement, Satellite navigation systems, Orbital Mechanics, Machine Learning, Automation