Design and simulation of a quad rotor tail-sitter unmanned aerial vehicle

Atsushi Oosedo, A. Konno, Takaaki Matumoto, Kenta Go, Kouji Masuko, S. Abiko, M. Uchiyama
{"title":"Design and simulation of a quad rotor tail-sitter unmanned aerial vehicle","authors":"Atsushi Oosedo, A. Konno, Takaaki Matumoto, Kenta Go, Kouji Masuko, S. Abiko, M. Uchiyama","doi":"10.1109/SII.2010.5708334","DOIUrl":null,"url":null,"abstract":"In this paper, we present the design and concept of a quad rotor tail-sitter UAV (unmanned aerial vehicle). The designed UAV is composed of quad rotors and a fixed wing. It can hover like a helicopter, and can cruise like a fixed wing airplane. In order to verify this concept, a simulator of a quad rotor tail-sitter UAV is developed. Simulation results show the advantage in energy efficiency of the proposed UAV over a conventional quad rotor helicopter type UAV. This paper also describes the development of the quad rotor tail-sitter UAV.","PeriodicalId":334652,"journal":{"name":"2010 IEEE/SICE International Symposium on System Integration","volume":"11 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2010-12-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"15","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"2010 IEEE/SICE International Symposium on System Integration","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/SII.2010.5708334","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 15

Abstract

In this paper, we present the design and concept of a quad rotor tail-sitter UAV (unmanned aerial vehicle). The designed UAV is composed of quad rotors and a fixed wing. It can hover like a helicopter, and can cruise like a fixed wing airplane. In order to verify this concept, a simulator of a quad rotor tail-sitter UAV is developed. Simulation results show the advantage in energy efficiency of the proposed UAV over a conventional quad rotor helicopter type UAV. This paper also describes the development of the quad rotor tail-sitter UAV.
四旋翼尾翼无人机的设计与仿真
本文提出了一种四旋翼尾翼无人机(UAV)的设计和概念。所设计的无人机由四旋翼和固定翼组成。它可以像直升机一样盘旋,也可以像固定翼飞机一样巡航。为了验证这一概念,开发了四旋翼尾翼无人机模拟器。仿真结果表明,与传统的四旋翼直升机型无人机相比,所提出的无人机在能效方面具有优势。本文还介绍了四旋翼尾翼无人机的研制情况。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
求助全文
约1分钟内获得全文 求助全文
来源期刊
自引率
0.00%
发文量
0
×
引用
GB/T 7714-2015
复制
MLA
复制
APA
复制
导出至
BibTeX EndNote RefMan NoteFirst NoteExpress
×
提示
您的信息不完整,为了账户安全,请先补充。
现在去补充
×
提示
您因"违规操作"
具体请查看互助需知
我知道了
×
提示
确定
请完成安全验证×
copy
已复制链接
快去分享给好友吧!
我知道了
右上角分享
点击右上角分享
0
联系我们:info@booksci.cn Book学术提供免费学术资源搜索服务,方便国内外学者检索中英文文献。致力于提供最便捷和优质的服务体验。 Copyright © 2023 布克学术 All rights reserved.
京ICP备2023020795号-1
ghs 京公网安备 11010802042870号
Book学术文献互助
Book学术文献互助群
群 号:481959085
Book学术官方微信