Satellite Attitude Control System Model Developed Using Simulink

I have developed a satellite attitude control system model using MATLAB Simulink. This model achieves precise satellite control by adjusting controller parameters and other system variables. The implementation includes PID controller blocks for attitude regulation, sensor modeling for data acquisition, and actuator modules for control signal execution. In this model, we have incorporated various satellite dynamics and environmental factors, such as orbital perturbations and torque disturbances, to better understand and predict satellite behavior. Through this simulation environment, we can conduct multiple experiments and simulations to optimize satellite attitude control algorithms using parameter tuning tools and custom MATLAB functions, thereby improving satellite stability and accuracy. These research activities and simulations are crucial for successful satellite missions, as a stable and precise attitude control system ensures satellites operate according to predetermined orbits and orientations, ultimately achieving various mission objectives.