Robotics and AI

Satellite Attitude Control using Reaction Wheels

This research presents a simulation of satellite attitude control using reaction wheels, a critical component in spacecraft engineering.

The model simulates a three-axis stabilized satellite equipped with reaction wheels, which adjust the satellite's orientation in space. The control system employs a Proportional-Integral-Derivative (PID) controller to manage the reaction wheels' torque, maintaining or changing the satellite’s attitude.

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