In our age, the most important technology that provides communication without selecting location and time is satellite communications undoubtedly. The antenna position control systems are used in providing that communication with high tracing accuracy. The goal of this study is to ensure the minimum angle deviation after the antenna is rotated. For this purpose, the antenna position control system is designed in MATLAB/Simulink and PID, fuzzy logic and sliding mode controllers are performed to the system. The simulation results are compared and the most suitable control method is determined.