The present application relates to the field of unmanned aerial vehicle (UAV) technologies, and provides a motor control system and a UAV. The motor control system includes a control unit, a first inverter electrically connected to the control unit, a second inverter electrically connected to the control unit, a first motor electrically connected to the first inverter and a second motor electrically connected to the second inverter. According to the foregoing manner, two inverters in the motor control system are electrically connected to one control unit. Therefore, the control unit can control running of two motors, thereby reducing the volume of a hardware circuit board having the motor control system and reducing the weight.
MOTOR CONTROL SYSTEM AND UNMANNED AERIAL VEHICLE
2020-09-10
Patent
Elektronische Ressource
Englisch
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