Novel tilting multi-rotor unmanned aerial vehicle platform
The invention discloses a novel tilting multi-rotor unmanned aerial vehicle platform, and belongs to the field of aircraft design and control. A fuselage of the multi-rotor unmanned aerial vehicle platform comprises a central equipment area and a fuselage carbon tube, wherein the fuselage carbon tub...
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| creator | LIU JINGDIAN WU HUIYI WU HAONAN CHENG BINGCHEN ZENG YIFAN YAN MAOCONG WANG SONG ZHANG NAN |
| description | The invention discloses a novel tilting multi-rotor unmanned aerial vehicle platform, and belongs to the field of aircraft design and control. A fuselage of the multi-rotor unmanned aerial vehicle platform comprises a central equipment area and a fuselage carbon tube, wherein the fuselage carbon tube comprises a transverse carbon tube connected with two vehicle arms and a tail arm carrying tail power; the left and right arms are made of carbon tubes, are respectively connected with transverse carbon tubes extending out of the left and right sides of the central equipment area, and can freely rotate around the transverse carbon tubes; a motor is arranged at each of the two ends of each arm; and a pair of coaxial reverse propeller mechanisms is arranged at the tail end of the tail arm. An arm and a fuselage of the unmanned aerial vehicle platform integrally form an H shape, and a tail arm and the fuselage integrally form a T shape. And the unmanned aerial vehicle platform realizes flight control by using a PID |
| format | Patent |
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A fuselage of the multi-rotor unmanned aerial vehicle platform comprises a central equipment area and a fuselage carbon tube, wherein the fuselage carbon tube comprises a transverse carbon tube connected with two vehicle arms and a tail arm carrying tail power; the left and right arms are made of carbon tubes, are respectively connected with transverse carbon tubes extending out of the left and right sides of the central equipment area, and can freely rotate around the transverse carbon tubes; a motor is arranged at each of the two ends of each arm; and a pair of coaxial reverse propeller mechanisms is arranged at the tail end of the tail arm. An arm and a fuselage of the unmanned aerial vehicle platform integrally form an H shape, and a tail arm and the fuselage integrally form a T shape. 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| language | chi ; eng |
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| subjects | AIRCRAFT AVIATION CONTROLLING COSMONAUTICS PERFORMING OPERATIONS PHYSICS REGULATING SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES TRANSPORTING |
| title | Novel tilting multi-rotor unmanned aerial vehicle platform |
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