Design and fabrication of a fixed-wing Unmanned Aerial Vehicle (UAV)

被引：19

作者：

El Adawy, Mohammed ^{[1
]}

Abdelhalim, Elhassan H. ^{[1
]}

Mahmoud, Mohannad ^{[1
]}

Zeid, Mohamed Ahmed Abo ^{[1
]}

Mohamed, Ibrahim H. ^{[1
]}

Othman, Mostafa M. ^{[1
]}

ElGamal, Gehad S. ^{[1
]}

ElShabasy, Yahia H. ^{[1
]}

机构：

[1] Alexandria Univ, Fac Engn, Mech Engn Dept, Alex 21544, Egypt

来源：

AIN SHAMS ENGINEERING JOURNAL | 2023年 / 14卷 / 09期

关键词：

Design; Fabrication; UAV; Wing; Tail; Fuselage; Performance analysis;

D O I：

10.1016/j.asej.2022.102094

中图分类号：

T [工业技术];

学科分类号：

08 ;

摘要：

Unmanned Aerial Vehicles (UAVs) have been widely used both in military and civil across the world in recent years. Nevertheless, their design always involves complex design optimization variables and deci-sions. Therefore, this paper aims to guide through the designing, manufacturing, and testing of an elec-trically powered radio-controlled aircraft for achieving a take-off, cruise, safe landing and carrying the highest payload possible. The whole process involves several phases, design phase, structural analysis, performance analysis, materials used, manufacturing, and finally aircraft testing. The final aircraft was designed with an empty weight and maximum take-off weight of 15.43 Ibs and 33.07 Ibs respectively while the wingspan, cruising speed and maximum speed were 70.1 in., 46 ft/s and 78 ft/sec respectively with a total take-off distance of 100 ft.(c) 2022 THE AUTHORS. Published by Elsevier BV on behalf of Faculty of Engineering, Ain Shams Uni-versity. This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/ by-nc-nd/4.0/).

引用

页数：17

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