Low altitude multi-rotor wing unmanned aerial vehicle system and control method thereof
A multi-rotor unmanned and unmanned aerial vehicle technology, which is applied to unmanned aircraft, aircraft, rotorcraft, etc., can solve the problems of inability to achieve exploration results, slow vertical take-off and landing speed, low work efficiency, etc. The effect of weight and vertical take-off and landing speed, improving work efficiency and good exploration effect
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[0034] In order to make the purpose, technical solutions and advantages of the embodiments of the present invention clearer, the technical solutions in the embodiments of the present invention will be clearly and completely described below in conjunction with the drawings in the embodiments of the present invention. Obviously, the described embodiments It is a part of embodiments of the present invention, but not all embodiments. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of the present invention.
[0035] figure 1 A schematic structural diagram of a low-altitude multi-rotor unmanned aerial vehicle system provided by an embodiment of the present invention, as figure 1 As shown, it includes: a flight control board 1, a brushless motor 2, a propeller 3 and an electronic regulator; Above, the brushless motor 2 is connected to the wing 5 corres...
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