Four-rotor aircraft outdoor formation light performance system and control method thereof
A technology of a quadrotor aircraft and a control method, which is applied in the direction of light control, non-electric variable control, control/regulation system, etc., can solve the problem of limited communication capability, low GPS positioning accuracy, and insufficient application of quadrotor aircraft formation performances, etc. The problem is to reduce the GPS measurement error, facilitate control, and reduce the low GPS positioning accuracy.
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[0036] The present invention will be described in detail below according to the accompanying drawings.
[0037] The formation light show system is mainly composed of three parts: the quadrotor aircraft unit performing formation flight missions, the host computer for data monitoring and command sending, and the communication system connecting the aircraft and the host computer.
[0038] Such as figure 1 As shown, the quadrotor unit consists of three parts: mechanical frame, power structure and control system.
[0039] The main body of the mechanical frame is the frame, which serves as the mechanical hardware carrying the power structure device and control device.
[0040] The power structure includes electronic governor, motor, battery and propeller, etc. The electronic governor receives the PWM wave from the flight controller, calculates the speed of the motor, and supplies the corresponding voltage to the motor to make the motor rotate and drive the propeller on the motor R...
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