The invention discloses an attitude correction
control system and method of a four-rotor aircraft. The
control system comprises a flight control main controller, a flight attitude acquisition module,a driving module, a
wireless communication module, a GPS module, a
power management module and a
camera module. The flight attitude acquisition module, the driving module, the
wireless communication module, the GPS module, the
power management module and the
camera module are connected with the flight control main controller. An unmanned aerial vehicle
attitude control system comprises a sensor data resolving and
processing system, a motor rotating
speed control system and a
wireless data communication
system. According to the invention,
cascade PID closed-
loop control is carried out on the attitude of the four-rotor aircraft, so that the PWM duty ratio for controlling the rotating speed of the motor is adjusted; and meanwhile, the four-rotor aircraft feeds back the position information obtained from the GPS module and current attitude data of the aircraft to a
remote control terminal through a wireless transceiving module, so that the operator checks the current flight state of the aircraft in real time and thus descending
processing is performed timely in an abnormal state of the flight to minimize the losses.