UAV flight control system is its "brain", including sensors, airborne computers and servo actuation equipment, to achieve
attitude stabilization, mission management and emergency control. It is mainly composed of gyroscope, acceleration
sensor, air pressure sensor, ultrasonic sensor, GPS module, etc. It is used to automatically maintain the normal flight attitude
of the aircraft. The IMU is used for attitude detection and measurement and transmitting data to the main control processor
MCU controls the stable operation of the aircraft through the flight algorithm.