Design Analysis of Solar-Powered Unmanned Aerial Vehicle
Autor(a) principal: | |
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Data de Publicação: | 2016 |
Outros Autores: | , , |
Tipo de documento: | Artigo |
Idioma: | eng |
Título da fonte: | Journal of Aerospace Technology and Management (Online) |
Texto Completo: | http://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462016000400397 |
Resumo: | ABSTRACT One of the main problems in micro unmanned aerial vehicles is endurance or flight time since the general domain aircraft uses conventional fuel, which is a pollutant, has a limited life and is costly. Then, there is a huge demand for using an unlimited non-exhaustible source of energy. Solar energy is one of the unlimited available renewable energy which can be used to increase the endurance of unmanned aerial vehicle without adding significant mass or increasing the size of the fuel system. This paper aims to encourage research on renewable energy sources for aviation considering the basic challenges for a solar-powered aircraft: geographical area of operation, energy collection and storage, payload and design parameters. Hence, a plane is designed for 2 kg, including payload, and is analyzed in various aspects. Besides, the design is optimized starting from airfoil to complete structure for better performance. |
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Design Analysis of Solar-Powered Unmanned Aerial VehicleSolar cellUnmanned aerial vehicleRenewable energyEnduranceConceptual designABSTRACT One of the main problems in micro unmanned aerial vehicles is endurance or flight time since the general domain aircraft uses conventional fuel, which is a pollutant, has a limited life and is costly. Then, there is a huge demand for using an unlimited non-exhaustible source of energy. Solar energy is one of the unlimited available renewable energy which can be used to increase the endurance of unmanned aerial vehicle without adding significant mass or increasing the size of the fuel system. This paper aims to encourage research on renewable energy sources for aviation considering the basic challenges for a solar-powered aircraft: geographical area of operation, energy collection and storage, payload and design parameters. Hence, a plane is designed for 2 kg, including payload, and is analyzed in various aspects. Besides, the design is optimized starting from airfoil to complete structure for better performance.Departamento de Ciência e Tecnologia Aeroespacial2016-12-01info:eu-repo/semantics/articleinfo:eu-repo/semantics/publishedVersiontext/htmlhttp://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462016000400397Journal of Aerospace Technology and Management v.8 n.4 2016reponame:Journal of Aerospace Technology and Management (Online)instname:Departamento de Ciência e Tecnologia Aeroespacial (DCTA)instacron:DCTA10.5028/jatm.v8i4.666info:eu-repo/semantics/openAccessSri,Karthik Reddy BuchireddyAneesh,PoondlaBhanu,KiranNatarajan,Meng2016-11-25T00:00:00Zoai:scielo:S2175-91462016000400397Revistahttp://www.jatm.com.br/ONGhttps://old.scielo.br/oai/scielo-oai.php||secretary@jatm.com.br2175-91461984-9648opendoar:2016-11-25T00:00Journal of Aerospace Technology and Management (Online) - Departamento de Ciência e Tecnologia Aeroespacial (DCTA)false |
dc.title.none.fl_str_mv |
Design Analysis of Solar-Powered Unmanned Aerial Vehicle |
title |
Design Analysis of Solar-Powered Unmanned Aerial Vehicle |
spellingShingle |
Design Analysis of Solar-Powered Unmanned Aerial Vehicle Sri,Karthik Reddy Buchireddy Solar cell Unmanned aerial vehicle Renewable energy Endurance Conceptual design |
title_short |
Design Analysis of Solar-Powered Unmanned Aerial Vehicle |
title_full |
Design Analysis of Solar-Powered Unmanned Aerial Vehicle |
title_fullStr |
Design Analysis of Solar-Powered Unmanned Aerial Vehicle |
title_full_unstemmed |
Design Analysis of Solar-Powered Unmanned Aerial Vehicle |
title_sort |
Design Analysis of Solar-Powered Unmanned Aerial Vehicle |
author |
Sri,Karthik Reddy Buchireddy |
author_facet |
Sri,Karthik Reddy Buchireddy Aneesh,Poondla Bhanu,Kiran Natarajan,M |
author_role |
author |
author2 |
Aneesh,Poondla Bhanu,Kiran Natarajan,M |
author2_role |
author author author |
dc.contributor.author.fl_str_mv |
Sri,Karthik Reddy Buchireddy Aneesh,Poondla Bhanu,Kiran Natarajan,M |
dc.subject.por.fl_str_mv |
Solar cell Unmanned aerial vehicle Renewable energy Endurance Conceptual design |
topic |
Solar cell Unmanned aerial vehicle Renewable energy Endurance Conceptual design |
description |
ABSTRACT One of the main problems in micro unmanned aerial vehicles is endurance or flight time since the general domain aircraft uses conventional fuel, which is a pollutant, has a limited life and is costly. Then, there is a huge demand for using an unlimited non-exhaustible source of energy. Solar energy is one of the unlimited available renewable energy which can be used to increase the endurance of unmanned aerial vehicle without adding significant mass or increasing the size of the fuel system. This paper aims to encourage research on renewable energy sources for aviation considering the basic challenges for a solar-powered aircraft: geographical area of operation, energy collection and storage, payload and design parameters. Hence, a plane is designed for 2 kg, including payload, and is analyzed in various aspects. Besides, the design is optimized starting from airfoil to complete structure for better performance. |
publishDate |
2016 |
dc.date.none.fl_str_mv |
2016-12-01 |
dc.type.driver.fl_str_mv |
info:eu-repo/semantics/article |
dc.type.status.fl_str_mv |
info:eu-repo/semantics/publishedVersion |
format |
article |
status_str |
publishedVersion |
dc.identifier.uri.fl_str_mv |
http://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462016000400397 |
url |
http://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462016000400397 |
dc.language.iso.fl_str_mv |
eng |
language |
eng |
dc.relation.none.fl_str_mv |
10.5028/jatm.v8i4.666 |
dc.rights.driver.fl_str_mv |
info:eu-repo/semantics/openAccess |
eu_rights_str_mv |
openAccess |
dc.format.none.fl_str_mv |
text/html |
dc.publisher.none.fl_str_mv |
Departamento de Ciência e Tecnologia Aeroespacial |
publisher.none.fl_str_mv |
Departamento de Ciência e Tecnologia Aeroespacial |
dc.source.none.fl_str_mv |
Journal of Aerospace Technology and Management v.8 n.4 2016 reponame:Journal of Aerospace Technology and Management (Online) instname:Departamento de Ciência e Tecnologia Aeroespacial (DCTA) instacron:DCTA |
instname_str |
Departamento de Ciência e Tecnologia Aeroespacial (DCTA) |
instacron_str |
DCTA |
institution |
DCTA |
reponame_str |
Journal of Aerospace Technology and Management (Online) |
collection |
Journal of Aerospace Technology and Management (Online) |
repository.name.fl_str_mv |
Journal of Aerospace Technology and Management (Online) - Departamento de Ciência e Tecnologia Aeroespacial (DCTA) |
repository.mail.fl_str_mv |
||secretary@jatm.com.br |
_version_ |
1754732531335299072 |