Design And Implementation Of Hybrid Wing Unmanned Aerial Vehicle (UAV)
Download as PDF
DOI: 10.38007/Proceedings.0001548
Corresponding Author
Qiang Feng
Abstract
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.
Keywords
Hybrid Wing UAV; Design; Implementation