Wing deformation type bionic unmanned aerial aircraft and deformation control method
A technology of unmanned aerial vehicles and wings, which is applied in the field of unmanned aerial vehicles to achieve the effects of improving wind resistance and maneuverability, improving aerodynamic efficiency, and increasing flight stability
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[0016] The present invention will be further described in detail below with reference to the accompanying drawings and specific embodiments.
[0017] The present invention adopts the layout configuration scheme of wing body fusion and flying wing, which is composed of 6 major functional components. like figure 1 As shown, it consists of six functional components: propeller 1, fixed wing body fusion wing segment 2, telescopic wing segment 3, folding wing control mechanism 4, bionic wing 5 and stabilized tail segment 6. In addition to being the main load-bearing structure of the entire aircraft, the fixed-wing body fused wing segment 2 is mainly used to load electromechanical equipment such as power system, flight control system, deformable structure servo drive motor and payload. The propeller 1 and the fused wing segment 2 of the fixed wing body are mechanically connected at the head through a rotating shaft, and a DC motor provides a rotational driving force to control the r...
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