用于飞机事故受害者急救的四架飞行器的设计

Alif Habib Hidayatulloh, Indra Adji Sulstijono, Anhar Risnumawan, Nofria Hanafi
{"title":"用于飞机事故受害者急救的四架飞行器的设计","authors":"Alif Habib Hidayatulloh, Indra Adji Sulstijono, Anhar Risnumawan, Nofria Hanafi","doi":"10.1109/IES50839.2020.9231846","DOIUrl":null,"url":null,"abstract":"Accidents can happen in many kind of public transportation to all people. This main of this kind of accident is evacuate process of transportation accident like plane and ship, meanwhile the location of accident can not reach, in case like aircraft accident at mountain forest and shinking of ship in the middle of the sea. Exploration in the accident area will be difficult with terrain to access it from rescue team. Therefore UAV is needed, UAV must have capability to hover at deep forest and can cruise in the middle of ocean, so the rescue team can easily find it. The author design a quad plane with an estimation of the plane’s total weight is 4400 gram and have ability to hover using four vertical motor and cruise using one horizontal motor that placed in the behind of UAV. Whereas to make transition from hover mode to cruise mode it requires an airspeed sensor as the parameter to make transition so than the plane will not lose the lift force. From the results of flight tests, quad plane can make the transition from QHOVER mode to FBWA at 10 m/s, with an altitude at 34 meters, a flying distance of quad plane at 188 meters, and a maximum speed of quad plane is 25 m/s. The quad plane also able to release the payload in the form of first aid which is useful for providing first aid to survivors.","PeriodicalId":344685,"journal":{"name":"2020 International Electronics Symposium (IES)","volume":"08 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2020-09-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Design of Quad Plane UAV with Carrier Gripper for First Aid of Victims from Aircraft Accident\",\"authors\":\"Alif Habib Hidayatulloh, Indra Adji Sulstijono, Anhar Risnumawan, Nofria Hanafi\",\"doi\":\"10.1109/IES50839.2020.9231846\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"Accidents can happen in many kind of public transportation to all people. This main of this kind of accident is evacuate process of transportation accident like plane and ship, meanwhile the location of accident can not reach, in case like aircraft accident at mountain forest and shinking of ship in the middle of the sea. Exploration in the accident area will be difficult with terrain to access it from rescue team. Therefore UAV is needed, UAV must have capability to hover at deep forest and can cruise in the middle of ocean, so the rescue team can easily find it. The author design a quad plane with an estimation of the plane’s total weight is 4400 gram and have ability to hover using four vertical motor and cruise using one horizontal motor that placed in the behind of UAV. Whereas to make transition from hover mode to cruise mode it requires an airspeed sensor as the parameter to make transition so than the plane will not lose the lift force. From the results of flight tests, quad plane can make the transition from QHOVER mode to FBWA at 10 m/s, with an altitude at 34 meters, a flying distance of quad plane at 188 meters, and a maximum speed of quad plane is 25 m/s. The quad plane also able to release the payload in the form of first aid which is useful for providing first aid to survivors.\",\"PeriodicalId\":344685,\"journal\":{\"name\":\"2020 International Electronics Symposium (IES)\",\"volume\":\"08 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2020-09-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2020 International Electronics Symposium (IES)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/IES50839.2020.9231846\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2020 International Electronics Symposium (IES)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/IES50839.2020.9231846","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 0

摘要

对所有人来说,各种公共交通都可能发生事故。这类事故主要是飞机、船舶等交通运输事故的疏散过程,同时事故发生的地点无法到达,如飞机事故发生在山林中,船舶在海中沉没。由于地形复杂,救援队伍难以进入事故区域进行勘探。因此需要无人机,无人机必须具有在森林深处悬停的能力和在海洋中央巡航的能力,这样救援队才能很容易地找到它。作者设计了一架四轴飞机,估计飞机总重量为4400克,能够使用四个垂直电机悬停,并使用放置在无人机后面的一个水平电机巡航。而从悬停模式到巡航模式的转换需要一个空速传感器作为参数来进行转换,这样飞机才不会失去升力。从飞行试验结果来看,四翼飞机以10 m/s的速度从QHOVER模式过渡到FBWA模式,飞行高度为34 m,飞行距离为188 m,最大飞行速度为25 m/s。四轴飞机还能够以急救的形式释放有效载荷,这对于为幸存者提供急救是有用的。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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
Design of Quad Plane UAV with Carrier Gripper for First Aid of Victims from Aircraft Accident
Accidents can happen in many kind of public transportation to all people. This main of this kind of accident is evacuate process of transportation accident like plane and ship, meanwhile the location of accident can not reach, in case like aircraft accident at mountain forest and shinking of ship in the middle of the sea. Exploration in the accident area will be difficult with terrain to access it from rescue team. Therefore UAV is needed, UAV must have capability to hover at deep forest and can cruise in the middle of ocean, so the rescue team can easily find it. The author design a quad plane with an estimation of the plane’s total weight is 4400 gram and have ability to hover using four vertical motor and cruise using one horizontal motor that placed in the behind of UAV. Whereas to make transition from hover mode to cruise mode it requires an airspeed sensor as the parameter to make transition so than the plane will not lose the lift force. From the results of flight tests, quad plane can make the transition from QHOVER mode to FBWA at 10 m/s, with an altitude at 34 meters, a flying distance of quad plane at 188 meters, and a maximum speed of quad plane is 25 m/s. The quad plane also able to release the payload in the form of first aid which is useful for providing first aid to survivors.
求助全文
通过发布文献求助,成功后即可免费获取论文全文。 去求助
来源期刊
自引率
0.00%
发文量
0
期刊最新文献
IES 2020 Cover Page Performance Improvement Based on Modified Lossless Quantization (MLQ) for Secret Key Generation Extracted from Received Signal Strength Performance Analysis of Routing Protocols AODV, OLSR and DSDV on MANET using NS3 Particle Swarm Optimization Implementation as MPPT on Hybrid Power System Data Analytics Implementation for Surabaya City Emergency Center
×
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