| 摘要 |
A multi-rotor unmanned aerial vehicle comprises: a vehicle main body which has a flying control part for controlling the flying of the multi-rotor unmanned aerial vehicle; first rotor parts which are connected to the vehicle main body according to the flying direction of the vehicle main body; and second rotor parts which are connected to the vehicle main body to be arranged between the first rotor parts, wherein the distance from the center of the vehicle main body to the rotation center of the first rotor parts is longer than the distance from the center of the vehicle main body to the rotation center of the second rotor parts, thereby increasing the flight duration thereof and improving the response ability to disturbance. |
