The present application relates to the field of unmanned aerial
vehicle control, in particular to a rotor unmanned aerial
vehicle control method based on lift feedback, the rotor unmanned aerial
vehicle control method based on lift feedback includes designing unmanned aerial vehicle control framework with lift feedback power
system and lift
closed loop controller based on rotor lift model and motor electric
governor model. First, remove the
motor speed inverse solution module in the traditional power
system in the unmanned aerial vehicle control framework, increase the lift
feedback control module, use the sensor to measure the lift generated by the rotor, realize
closed loop control;Second, the power
system model of multi-rotor unmanned aerial vehicle is established, the motor
throttle is taken as the input, and the rotor lift is taken as the output;Finally, based on this model, the input-output
linearization force
closed loop controller is designed to accurately control the lift output. The method solves the problems of low control accuracy and poor
flight stability of the rotor unmanned aerial vehicle in the
wind disturbance environment operation or maneuvering
flight process. By applying this control method to the rotor unmanned aerial vehicle to ensure its high precision control and stable flight in the
wind disturbance environment and maneuvering
flight process.