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Design and implementation of a VTOL flight transition mechanism and development of a mathematical model for a tilt rotor UAV

In the last decade, the interest in the development of unmanned aerial vehicles and the implementation of different flight topologies have been justified mainly by a wide range of applications, both military and civil. The current work can be used for educational purposes and we present two approach...

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第一著者: Paiva, Enrique (author)
その他の著者: Llano, Marcelo (author), Rodas Benítez, Jorge Esteban (author), Gregor Recalde, Raúl Igmar (author), Rodríguez Piñeiro, José (author), Gómez, Marcos (author)
フォーマット: article
言語:英語
出版事項: 2018
主題:
4. Transporte, telecomunicaciones y otras infraestructuras
UNMANNED AERIAL VEHICLE (UAV)
HYBRID UAV MATHEMATICAL MODEL
TRI-ROTOR
FIXED-WING
VERTICAL TAKEOFF AND LANDING (VTOL)
INGENIERIA
オンライン･アクセス:http://hdl.handle.net/20.500.14066/3642
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author Paiva, Enrique
author2 Llano, Marcelo
Rodas Benítez, Jorge Esteban
Gregor Recalde, Raúl Igmar
Rodríguez Piñeiro, José
Gómez, Marcos
author2_role author
author
author
author
author
author_browse Gregor Recalde, Raúl Igmar
Gómez, Marcos
Llano, Marcelo
Paiva, Enrique
Rodas Benítez, Jorge Esteban
Rodríguez Piñeiro, José
author_facet Paiva, Enrique
Llano, Marcelo
Rodas Benítez, Jorge Esteban
Gregor Recalde, Raúl Igmar
Rodríguez Piñeiro, José
Gómez, Marcos
author_role author
bitstream.checksum.fl_str_mv 494b7804f710b9ffcda086f089ade05b
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bitstream.url.fl_str_mv http://repositorio.conacyt.gov.py/bitstream/20.500.14066/3642/1/PINV15-136art5.pdf
http://repositorio.conacyt.gov.py/bitstream/20.500.14066/3642/2/license.txt
http://repositorio.conacyt.gov.py/bitstream/20.500.14066/3642/3/PINV15-136art5.pdf.txt
dc.contributor.other.es.fl_str_mv Universidad Nacional de Asunción - Facultad de Ingeniería
dc.creator.none.fl_str_mv Paiva, Enrique
Llano, Marcelo
Rodas Benítez, Jorge Esteban
Gregor Recalde, Raúl Igmar
Rodríguez Piñeiro, José
Gómez, Marcos
dc.date.accessioned.none.fl_str_mv 2022-04-25T22:41:20Z
dc.date.available.none.fl_str_mv 2022-04-25T22:41:20Z
dc.date.issued.none.fl_str_mv 2018
dc.identifier.uri.none.fl_str_mv http://hdl.handle.net/20.500.14066/3642
dc.language.iso.es.fl_str_mv eng
dc.relation.projectCONACYT.es.fl_str_mv PINV15-136
dc.rights.accessRights.es.fl_str_mv info:eu-repo/semantics/openAccess
dc.subject.classification.es.fl_str_mv 4. Transporte, telecomunicaciones y otras infraestructuras
dc.subject.ocde.es.fl_str_mv INGENIERIA
dc.subject.other.es.fl_str_mv UNMANNED AERIAL VEHICLE (UAV)
HYBRID UAV MATHEMATICAL MODEL
TRI-ROTOR
FIXED-WING
VERTICAL TAKEOFF AND LANDING (VTOL)
dc.title.es.fl_str_mv Design and implementation of a VTOL flight transition mechanism and development of a mathematical model for a tilt rotor UAV
dc.type.es.fl_str_mv info:eu-repo/semantics/article
info:eu-repo/semantics/publishedVersion
description In the last decade, the interest in the development of unmanned aerial vehicles and the implementation of different flight topologies have been justified mainly by a wide range of applications, both military and civil. The current work can be used for educational purposes and we present two approaches in this area.
eu_rights_str_mv openAccess
format article
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language eng
network_acronym_str CONACYT
network_name_str Repositorio Institucional CONACYT
oai_identifier_str oai:repositorio.conacyt.gov.py:20.500.14066/3642
publishDate 2018
publishDateSort 2018
repository.mail.fl_str_mv repositorio.institucional@conacyt.gov.py
repository.name.fl_str_mv Repositorio Institucional CONACYT
repository_id_str
spelling 74ebcfee-142c-4f2b-9b20-48364ad54cf06009e2c5fbf-384b-4830-a3bb-5d6dcd3f0ef06009756005696000000-0002-7717-4100903600df4a917c-5e00-4154-8ffd-44f81939fb45600Universidad Nacional de Asunción - Facultad de Ingeniería2022-04-25T22:41:20Z2022-04-25T22:41:20Z2018http://hdl.handle.net/20.500.14066/3642In the last decade, the interest in the development of unmanned aerial vehicles and the implementation of different flight topologies have been justified mainly by a wide range of applications, both military and civil. The current work can be used for educational purposes and we present two approaches in this area.Consejo Nacional de Ciencia y TecnologíaPROCIENCIAeng4. Transporte, telecomunicaciones y otras infraestructurasUNMANNED AERIAL VEHICLE (UAV)HYBRID UAV MATHEMATICAL MODELTRI-ROTORFIXED-WINGVERTICAL TAKEOFF AND LANDING (VTOL)INGENIERIADesign and implementation of a VTOL flight transition mechanism and development of a mathematical model for a tilt rotor UAVinfo:eu-repo/semantics/articleinfo:eu-repo/semantics/publishedVersionPINV15-136info:eu-repo/semantics/openAccessPaiva, EnriqueLlano, MarceloRodas Benítez, Jorge EstebanGregor Recalde, Raúl IgmarRodríguez Piñeiro, JoséGómez, MarcosORIGINALPINV15-136art5.pdfPINV15-136art5.pdfapplication/pdf2999459http://repositorio.conacyt.gov.py/bitstream/20.500.14066/3642/1/PINV15-136art5.pdf494b7804f710b9ffcda086f089ade05bMD51LICENSElicense.txtlicense.txttext/plain; charset=utf-81698http://repositorio.conacyt.gov.py/bitstream/20.500.14066/3642/2/license.txt858b22fda432bd774e469302988c1974MD52TEXTPINV15-136art5.pdf.txtPINV15-136art5.pdf.txtExtracted texttext/plain25866http://repositorio.conacyt.gov.py/bitstream/20.500.14066/3642/3/PINV15-136art5.pdf.txte3de558bb090b87e360c4e066e8454fdMD5320.500.14066/3642oai:repositorio.conacyt.gov.py:20.500.14066/36422026-02-12 19:30:29.513Repositorio Institucional CONACYTrepositorio.institucional@conacyt.gov.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
spellingShingle Design and implementation of a VTOL flight transition mechanism and development of a mathematical model for a tilt rotor UAV
Paiva, Enrique
4. Transporte, telecomunicaciones y otras infraestructuras
UNMANNED AERIAL VEHICLE (UAV)
HYBRID UAV MATHEMATICAL MODEL
TRI-ROTOR
FIXED-WING
VERTICAL TAKEOFF AND LANDING (VTOL)
INGENIERIA
status_str publishedVersion
title Design and implementation of a VTOL flight transition mechanism and development of a mathematical model for a tilt rotor UAV
title_full Design and implementation of a VTOL flight transition mechanism and development of a mathematical model for a tilt rotor UAV
title_fullStr Design and implementation of a VTOL flight transition mechanism and development of a mathematical model for a tilt rotor UAV
title_full_unstemmed Design and implementation of a VTOL flight transition mechanism and development of a mathematical model for a tilt rotor UAV
title_short Design and implementation of a VTOL flight transition mechanism and development of a mathematical model for a tilt rotor UAV
title_sort Design and implementation of a VTOL flight transition mechanism and development of a mathematical model for a tilt rotor UAV
topic 4. Transporte, telecomunicaciones y otras infraestructuras
UNMANNED AERIAL VEHICLE (UAV)
HYBRID UAV MATHEMATICAL MODEL
TRI-ROTOR
FIXED-WING
VERTICAL TAKEOFF AND LANDING (VTOL)
INGENIERIA
url http://hdl.handle.net/20.500.14066/3642

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