Kite Sky Anchor Analysis for Drone Launching System

M. Rossett
{"title":"Kite Sky Anchor Analysis for Drone Launching System","authors":"M. Rossett","doi":"10.4172/2168-9792.1000156","DOIUrl":null,"url":null,"abstract":"A system was developed to launch unmanned aerial vehicles (UAV) near cruising altitude by utilizing a kite based system. A kite was flown in the sky asking as an anchor in the sky. A UAV was brought up the tether and released. The tension, tether angles, and other flight characteristics of the kite were simulated and field tested. This data was used to determine the feasibility of the overall project.","PeriodicalId":356774,"journal":{"name":"Journal of Aeronautics and Aerospace Engineering","volume":"47 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2016-01-22","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Journal of Aeronautics and Aerospace Engineering","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.4172/2168-9792.1000156","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 0

Abstract

A system was developed to launch unmanned aerial vehicles (UAV) near cruising altitude by utilizing a kite based system. A kite was flown in the sky asking as an anchor in the sky. A UAV was brought up the tether and released. The tension, tether angles, and other flight characteristics of the kite were simulated and field tested. This data was used to determine the feasibility of the overall project.
查看原文
分享 分享
微信好友 朋友圈 QQ好友 复制链接
本刊更多论文
无人机发射系统风筝天空锚分析
开发了一种利用风筝为基础的系统在巡航高度附近发射无人机(UAV)的系统。一只风筝在天空中飞翔,像天空中的锚一样。一架无人机被拉上缆绳并释放。对风筝的张力、系绳角度和其他飞行特性进行了模拟和现场测试。这些数据被用来确定整个项目的可行性。
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 去求助
来源期刊
自引率
0.00%
发文量
0
期刊最新文献
Mechanical Behavior of a Fuselage Stiffened Carbon-Epoxy Panel under Debonding Load On the Modeling of Light Aircraft Landing Gears Various aspects of situation awareness with respect to human-machine-interaction while using optoavionic cockpit instrumentation in aircraft Autopilot Design of Unmanned Aerial Vehicle A New Methodology for Aerodynamic Design and Analysis of a Small Scale Blended Wing Body
×
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
现在去查看 取消
×
提示
确定
0
微信
客服QQ
Book学术公众号 扫码关注我们
反馈
×
意见反馈
请填写您的意见或建议
请填写您的手机或邮箱
已复制链接
已复制链接
快去分享给好友吧!
我知道了
×
扫码分享
扫码分享
Book学术官方微信
Book学术文献互助
Book学术文献互助群
群 号:481959085
Book学术
文献互助 智能选刊 最新文献 互助须知 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 Book学术 All rights reserved.
ghs 京公网安备 11010802042870号 京ICP备2023020795号-1