Vertical take-off and landing fixed-wing unmanned aerial vehicle
A vertical take-off and landing, fixed-wing technology, applied in the field of unmanned aerial vehicles, can solve the problems of difficult to control the balance of the body, high overall cost, large space occupied by the rotor, etc. Effect
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[0043] In the present invention, the orientation of the body 1 is used for illustration, that is, figure 1 For example, the head of the body 1 is the front, the tail is the rear, and the upper part of the body 1 is the top. The accompanying drawings in the present invention are all schematic diagrams. For the convenience of observation, some auxiliary structures are omitted, and only some structures related to the present invention are highlighted, which are some structures that are specially noted, and are commonly used structures in the prior art.
[0044] like figure 1 , 2Among them, a vertical take-off and landing fixed-wing UAV includes a fuselage 2, wings 5 are provided on both sides of the fuselage 2, and a forward drive is provided on the fuselage 1. The forward drive described in this example, That is due to the device driving the whole body 1 to fly forward, including such as figure 1 The front rotor 10 shown in , or be located at the rotor below the wing or ahe...
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