The unmanned aerial vehicle having a multi-degree-of-freedom flight mode according to the present invention comprises: a fuselage unit having a battery attached thereto and having a forward direction set as an x-axis; more than four rotors are arranged around the fuselage part, and the rotating shafts of the rotors are arranged in order in the z-axis direction; an x-axis tilting mechanism unit that tilts the plurality of rotors about respective axes parallel to the x-axis; a y-axis tilting mechanism unit that tilts the plurality of rotors about respective axes parallel to the y-axis; and a first drive motor unit for driving the y-axis tilting mechanism unit. A second drive motor unit for driving the x-axis tilting mechanism unit; and a control unit that implements a plurality of flight modes by controlling the first rotor, the second rotor, the third rotor, the fourth rotor, the first drive motor unit, and the second drive motor unit.
本发明的具有多自由度飞行模式的无人机包括:机身部,安装有电池,前进方向被设定为x轴;多个旋翼,在所述机身部的周围设置有四个以上,各个旋转轴向z轴方向整齐排列;x轴倾斜机构部,使所述多个旋翼以平行于所述x轴的各个轴为中心而倾斜;y轴倾斜机构部,使所述多个旋翼以平行于y轴的各个轴为中心而倾斜;及第一驱动马达部,用于驱动所述y轴倾斜机构部;第二驱动马达部,用于驱动所述x轴倾斜机构部;及控制部,控制所述第一旋翼、所述第二旋翼、所述第三旋翼、所述第四旋翼、所述第一驱动马达部及所述第二驱动马达部而实现多个飞行模式。
Unmanned aerial vehicle with multi-degree-of-freedom flight mode
具有多自由度飞行模式的无人机
2023-03-03
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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