Motion Equations and Attitude Control in the Vertical Flight of a VTOL Bi-Rotor UAV: Part 2

[EN] This paper gathers the dynamical modeling of an unmanned aircraft and the design and simulation of the control system, allowing it to perform a Vertical Take-Off (VTOL) maneuver, a fixed-wing (FW) flight and a transition between the two configurations using two tilting rotors (Bi-Tilt). These U...

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Detalles Bibliográficos
Autores: Musoles, Jose Luis, Garcia-Nieto, Sergio, Simarro Fernández, Raúl|||0000-0002-7311-2025, Ramos Fernández, César|||0000-0003-1806-2114
Tipo de recurso: artículo
Fecha de publicación:2024
País:España
Institución:Universitat Politècnica de València (UPV)
Repositorio:RiuNet. Repositorio Institucional de la Universitat Politécnica de Valéncia
Idioma:inglés
OAI Identifier:oai:riunet.upv.es:10251/207937
Acceso en línea:https://riunet.upv.es/handle/10251/207937
Access Level:acceso abierto
Palabra clave:Tilt rotors
Non-linear dynamics
Simulation
Vertical take-off
Fixed wing
Aerodynamics
INGENIERIA DE SISTEMAS Y AUTOMATICA
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spelling Motion Equations and Attitude Control in the Vertical Flight of a VTOL Bi-Rotor UAV: Part 2Musoles, Jose LuisGarcia-Nieto, SergioSimarro Fernández, Raúl|||0000-0002-7311-2025Ramos Fernández, César|||0000-0003-1806-2114Tilt rotorsNon-linear dynamicsSimulationVertical take-offFixed wingAerodynamicsINGENIERIA DE SISTEMAS Y AUTOMATICA[EN] This paper gathers the dynamical modeling of an unmanned aircraft and the design and simulation of the control system, allowing it to perform a Vertical Take-Off (VTOL) maneuver, a fixed-wing (FW) flight and a transition between the two configurations using two tilting rotors (Bi-Tilt). These Unmanned Aerial Vehicles (UAVs) operating in this configuration are categorized as Hybrid UAVs, for their capability of having a dual flight envelope: flying like a multi-rotor and navigating like a traditional fixed-wing aircraft, allowing the drone to perform complex missions where these two flight configurations are essential. This work exhibits the Bi-Rotor non-linear dynamics, valid for both flight configurations, the design of the control algorithm for stability and navigation, and a simulation of a complete flight mission.This work has been supported by the Spain government via MCIN/AEI/10.13039/501100011033 [Project PID2020-119468RA-I00].MDPI AGDepartamento de Ingeniería de Sistemas y AutomáticaInstituto Universitario de Automática e Informática IndustrialEscuela Técnica Superior de Ingeniería IndustrialAgencia Estatal de InvestigaciónRepositorio Institucional de la Universitat Politècnica de València Riunet20242024-07-01journal articlehttp://purl.org/coar/resource_type/c_6501VoRhttp://purl.org/coar/version/c_970fb48d4fbd8a85info:eu-repo/semantics/articleapplication/pdfhttps://riunet.upv.es/handle/10251/207937reponame:RiuNet. Repositorio Institucional de la Universitat Politécnica de Valénciainstname:Universitat Politècnica de València (UPV)InglésengAgencia Estatal de Investigación http://dx.doi.org/10.13039/501100011033 Plan Estatal de Investigación Científica y Técnica y de Innovación 2017-2020 PID2020-119468RA-I00 DISEÑO, CONSTRUCCION Y CONTROL PARA LA GESTION OPTIMA DE MISIONES EN AERONAVES NO TRIPULADAS (UAVS) DE RANGO EXTENDIDO BASADAS EN PILA DE HIDROGENO Y PROPULSION DISTRIBUIDAopen accesshttp://purl.org/coar/access_right/c_abf2Reconocimiento (by)http://creativecommons.org/licenses/by/4.0/info:eu-repo/semantics/openAccessoai:riunet.upv.es:10251/2079372026-06-13T07:49:27Z
dc.title.none.fl_str_mv Motion Equations and Attitude Control in the Vertical Flight of a VTOL Bi-Rotor UAV: Part 2
title Motion Equations and Attitude Control in the Vertical Flight of a VTOL Bi-Rotor UAV: Part 2
spellingShingle Motion Equations and Attitude Control in the Vertical Flight of a VTOL Bi-Rotor UAV: Part 2
Musoles, Jose Luis
Tilt rotors
Non-linear dynamics
Simulation
Vertical take-off
Fixed wing
Aerodynamics
INGENIERIA DE SISTEMAS Y AUTOMATICA
title_short Motion Equations and Attitude Control in the Vertical Flight of a VTOL Bi-Rotor UAV: Part 2
title_full Motion Equations and Attitude Control in the Vertical Flight of a VTOL Bi-Rotor UAV: Part 2
title_fullStr Motion Equations and Attitude Control in the Vertical Flight of a VTOL Bi-Rotor UAV: Part 2
title_full_unstemmed Motion Equations and Attitude Control in the Vertical Flight of a VTOL Bi-Rotor UAV: Part 2
title_sort Motion Equations and Attitude Control in the Vertical Flight of a VTOL Bi-Rotor UAV: Part 2
dc.creator.none.fl_str_mv Musoles, Jose Luis
Garcia-Nieto, Sergio
Simarro Fernández, Raúl|||0000-0002-7311-2025
Ramos Fernández, César|||0000-0003-1806-2114
author Musoles, Jose Luis
author_facet Musoles, Jose Luis
Garcia-Nieto, Sergio
Simarro Fernández, Raúl|||0000-0002-7311-2025
Ramos Fernández, César|||0000-0003-1806-2114
author_role author
author2 Garcia-Nieto, Sergio
Simarro Fernández, Raúl|||0000-0002-7311-2025
Ramos Fernández, César|||0000-0003-1806-2114
author2_role author
author
author
dc.contributor.none.fl_str_mv Departamento de Ingeniería de Sistemas y Automática
Instituto Universitario de Automática e Informática Industrial
Escuela Técnica Superior de Ingeniería Industrial
Agencia Estatal de Investigación
Repositorio Institucional de la Universitat Politècnica de València Riunet
dc.subject.none.fl_str_mv Tilt rotors
Non-linear dynamics
Simulation
Vertical take-off
Fixed wing
Aerodynamics
INGENIERIA DE SISTEMAS Y AUTOMATICA
topic Tilt rotors
Non-linear dynamics
Simulation
Vertical take-off
Fixed wing
Aerodynamics
INGENIERIA DE SISTEMAS Y AUTOMATICA
description [EN] This paper gathers the dynamical modeling of an unmanned aircraft and the design and simulation of the control system, allowing it to perform a Vertical Take-Off (VTOL) maneuver, a fixed-wing (FW) flight and a transition between the two configurations using two tilting rotors (Bi-Tilt). These Unmanned Aerial Vehicles (UAVs) operating in this configuration are categorized as Hybrid UAVs, for their capability of having a dual flight envelope: flying like a multi-rotor and navigating like a traditional fixed-wing aircraft, allowing the drone to perform complex missions where these two flight configurations are essential. This work exhibits the Bi-Rotor non-linear dynamics, valid for both flight configurations, the design of the control algorithm for stability and navigation, and a simulation of a complete flight mission.
publishDate 2024
dc.date.none.fl_str_mv 2024
2024-07-01
dc.type.none.fl_str_mv journal article
http://purl.org/coar/resource_type/c_6501
VoR
http://purl.org/coar/version/c_970fb48d4fbd8a85
dc.type.openaire.fl_str_mv info:eu-repo/semantics/article
format article
dc.identifier.none.fl_str_mv https://riunet.upv.es/handle/10251/207937
url https://riunet.upv.es/handle/10251/207937
dc.language.none.fl_str_mv Inglés
eng
language_invalid_str_mv Inglés
language eng
dc.relation.none.fl_str_mv Agencia Estatal de Investigación http://dx.doi.org/10.13039/501100011033 Plan Estatal de Investigación Científica y Técnica y de Innovación 2017-2020 PID2020-119468RA-I00 DISEÑO, CONSTRUCCION Y CONTROL PARA LA GESTION OPTIMA DE MISIONES EN AERONAVES NO TRIPULADAS (UAVS) DE RANGO EXTENDIDO BASADAS EN PILA DE HIDROGENO Y PROPULSION DISTRIBUIDA
dc.rights.none.fl_str_mv open access
http://purl.org/coar/access_right/c_abf2
Reconocimiento (by)
http://creativecommons.org/licenses/by/4.0/
dc.rights.openaire.fl_str_mv info:eu-repo/semantics/openAccess
rights_invalid_str_mv open access
http://purl.org/coar/access_right/c_abf2
Reconocimiento (by)
http://creativecommons.org/licenses/by/4.0/
eu_rights_str_mv openAccess
dc.format.none.fl_str_mv application/pdf
dc.publisher.none.fl_str_mv MDPI AG
publisher.none.fl_str_mv MDPI AG
dc.source.none.fl_str_mv reponame:RiuNet. Repositorio Institucional de la Universitat Politécnica de Valéncia
instname:Universitat Politècnica de València (UPV)
instname_str Universitat Politècnica de València (UPV)
reponame_str RiuNet. Repositorio Institucional de la Universitat Politécnica de Valéncia
collection RiuNet. Repositorio Institucional de la Universitat Politécnica de Valéncia
repository.name.fl_str_mv
repository.mail.fl_str_mv
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score 15,811543

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