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Design And Implementation Of Hybrid Wing Unmanned Aerial Vehicle (UAV)

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DOI: 10.38007/Proceedings.0001548


Qiang Feng

Corresponding Author

Qiang Feng


This paper designs a hybrid wing UAV based on the study of existing UAV modes and functions, and elaborates its functional implementation requirements and design possibilities in detail. It is hoped to be beneficial to the development of UAV to achieve the goal of energy saving and consumption reduction.


Hybrid Wing UAV; Design; Implementation