Conceptual Design of a Cargo UAV That Can Take-off and Land Vertically

2021 3rd International Congress on Human-Computer Interaction, Optimization and Robotic Applications (HORA) Pub Date : 2021-06-11 DOI:10.1109/HORA52670.2021.9461393

Sezgin Yolcu, M. Akdağ

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Abstract

Fixed-wing vertical take-off and landing (VTOL) unmanned aerial vehicle (UAV)s are designed to combine the advantages of multi-rotor UAVs and fixed-wing UAVs in different flight phases in a single UAV. Fixed-wing VTOL UAVs can achieve the mobility of multi-rotor UAVs in hovering, vertical take-off and landing flight phases. Since fixed-wing UAVs are known for their efficiency in power consumption, fixed-wing VTOL UAVs were created to efficiently perform the cruise phase of the flight for a similar reason. In this paper, we made the conceptual design of a fixed-wing VTOL UAV which is called “DOGA”. The mission of DOGA is to carry 0.5 kg. payload. Firstly, maximum take-off weight was calculated, and then the airfoil profile, wings geometry, and the propulsion systems were determined. Also, design and performance parameters of DOGA were calculated. As a result, conceptual design of DOGA was completed and all the needed parameters for the detail design of the fixed-wing VTOL UAV were derived.

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垂直起降货运无人机概念设计

固定翼垂直起降(VTOL)无人机是将多旋翼无人机和固定翼无人机在不同飞行阶段的优势结合在一架无人机上而设计的。固定翼垂直起降无人机可以实现多旋翼无人机在悬停、垂直起飞和降落飞行阶段的机动性。由于固定翼无人机以其功率消耗效率而闻名，固定翼垂直起降无人机的创建是为了有效地执行飞行的巡航阶段，原因类似。本文对一种固定翼垂直起降无人机“DOGA”进行了概念设计。DOGA的任务是携带0.5公斤。有效载荷。首先计算了最大起飞重量，然后确定了翼型轮廓、机翼几何形状和推进系统。同时，计算了DOGA的设计参数和性能参数。在此基础上，完成了垂直起降无人机的概念设计，并推导出了固定翼垂直起降无人机详细设计所需的参数。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

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2021 3rd International Congress on Human-Computer Interaction, Optimization and Robotic Applications (HORA)

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