Analysis of electro-hydrostatic actuator in more electric aircraft.

Detalhes bibliográficos
Autor(a) principal: Francival Barbosa Júnior
Data de Publicação: 2006
Tipo de documento: Dissertação
Idioma: eng
Título da fonte: Biblioteca Digital de Teses e Dissertações do ITA
Texto Completo: http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=900
Resumo: The aim of this dissertation is to evaluate the possibility of using electrically powered systems instead of a centralized hydraulic system composed of set of distribution pipes for aircrafts' primary control surfaces actuation. Focus will be given in the following topics: Description of new actuation technologies; Option chosen to be studied among the new possibilities; Comparison between the traditional system and the new proposal e System engineering evaluation regarding: weight, safety, thermal issue, connection with electric system, maintenance and certification. Besides that, a more electric actuation architecture will be proposed and compared with the conventional option for an airplane design's case study. A simulation model will be developed to describe the more electric actuator behavior and preview its interaction with other systems. This model will be included in a closed loop to command a primary surface. The closed-loop project will be developed based on an algorithmic method. A Genetic Algorithm (GA) will be implemented to define the gains. Finally, the results obtained will be discussed.
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spelling Analysis of electro-hydrostatic actuator in more electric aircraft.AtuadoresControle de pilotagem por fiosModelos matemáticosAlgoritmos genéticosControle automático de vôoProjeto de aeronavesSimulação computadorizadaSuperfícies de controleEngenharia aeronáuticaThe aim of this dissertation is to evaluate the possibility of using electrically powered systems instead of a centralized hydraulic system composed of set of distribution pipes for aircrafts' primary control surfaces actuation. Focus will be given in the following topics: Description of new actuation technologies; Option chosen to be studied among the new possibilities; Comparison between the traditional system and the new proposal e System engineering evaluation regarding: weight, safety, thermal issue, connection with electric system, maintenance and certification. Besides that, a more electric actuation architecture will be proposed and compared with the conventional option for an airplane design's case study. A simulation model will be developed to describe the more electric actuator behavior and preview its interaction with other systems. This model will be included in a closed loop to command a primary surface. The closed-loop project will be developed based on an algorithmic method. A Genetic Algorithm (GA) will be implemented to define the gains. Finally, the results obtained will be discussed.Instituto Tecnológico de AeronáuticaAlberto Adade FilhoMarcelo Santana ScrodenFrancival Barbosa Júnior2006-12-28info:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/masterThesishttp://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=900reponame:Biblioteca Digital de Teses e Dissertações do ITAinstname:Instituto Tecnológico de Aeronáuticainstacron:ITAenginfo:eu-repo/semantics/openAccessapplication/pdf2019-02-02T14:01:58Zoai:agregador.ibict.br.BDTD_ITA:oai:ita.br:900http://oai.bdtd.ibict.br/requestopendoar:null2020-05-28 19:34:38.161Biblioteca Digital de Teses e Dissertações do ITA - Instituto Tecnológico de Aeronáuticatrue
dc.title.none.fl_str_mv Analysis of electro-hydrostatic actuator in more electric aircraft.
title Analysis of electro-hydrostatic actuator in more electric aircraft.
spellingShingle Analysis of electro-hydrostatic actuator in more electric aircraft.
Francival Barbosa Júnior
Atuadores
Controle de pilotagem por fios
Modelos matemáticos
Algoritmos genéticos
Controle automático de vôo
Projeto de aeronaves
Simulação computadorizada
Superfícies de controle
Engenharia aeronáutica
title_short Analysis of electro-hydrostatic actuator in more electric aircraft.
title_full Analysis of electro-hydrostatic actuator in more electric aircraft.
title_fullStr Analysis of electro-hydrostatic actuator in more electric aircraft.
title_full_unstemmed Analysis of electro-hydrostatic actuator in more electric aircraft.
title_sort Analysis of electro-hydrostatic actuator in more electric aircraft.
author Francival Barbosa Júnior
author_facet Francival Barbosa Júnior
author_role author
dc.contributor.none.fl_str_mv Alberto Adade Filho
Marcelo Santana Scroden
dc.contributor.author.fl_str_mv Francival Barbosa Júnior
dc.subject.por.fl_str_mv Atuadores
Controle de pilotagem por fios
Modelos matemáticos
Algoritmos genéticos
Controle automático de vôo
Projeto de aeronaves
Simulação computadorizada
Superfícies de controle
Engenharia aeronáutica
topic Atuadores
Controle de pilotagem por fios
Modelos matemáticos
Algoritmos genéticos
Controle automático de vôo
Projeto de aeronaves
Simulação computadorizada
Superfícies de controle
Engenharia aeronáutica
dc.description.none.fl_txt_mv The aim of this dissertation is to evaluate the possibility of using electrically powered systems instead of a centralized hydraulic system composed of set of distribution pipes for aircrafts' primary control surfaces actuation. Focus will be given in the following topics: Description of new actuation technologies; Option chosen to be studied among the new possibilities; Comparison between the traditional system and the new proposal e System engineering evaluation regarding: weight, safety, thermal issue, connection with electric system, maintenance and certification. Besides that, a more electric actuation architecture will be proposed and compared with the conventional option for an airplane design's case study. A simulation model will be developed to describe the more electric actuator behavior and preview its interaction with other systems. This model will be included in a closed loop to command a primary surface. The closed-loop project will be developed based on an algorithmic method. A Genetic Algorithm (GA) will be implemented to define the gains. Finally, the results obtained will be discussed.
description The aim of this dissertation is to evaluate the possibility of using electrically powered systems instead of a centralized hydraulic system composed of set of distribution pipes for aircrafts' primary control surfaces actuation. Focus will be given in the following topics: Description of new actuation technologies; Option chosen to be studied among the new possibilities; Comparison between the traditional system and the new proposal e System engineering evaluation regarding: weight, safety, thermal issue, connection with electric system, maintenance and certification. Besides that, a more electric actuation architecture will be proposed and compared with the conventional option for an airplane design's case study. A simulation model will be developed to describe the more electric actuator behavior and preview its interaction with other systems. This model will be included in a closed loop to command a primary surface. The closed-loop project will be developed based on an algorithmic method. A Genetic Algorithm (GA) will be implemented to define the gains. Finally, the results obtained will be discussed.
publishDate 2006
dc.date.none.fl_str_mv 2006-12-28
dc.type.driver.fl_str_mv info:eu-repo/semantics/publishedVersion
info:eu-repo/semantics/masterThesis
status_str publishedVersion
format masterThesis
dc.identifier.uri.fl_str_mv http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=900
url http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=900
dc.language.iso.fl_str_mv eng
language eng
dc.rights.driver.fl_str_mv info:eu-repo/semantics/openAccess
eu_rights_str_mv openAccess
dc.format.none.fl_str_mv application/pdf
dc.publisher.none.fl_str_mv Instituto Tecnológico de Aeronáutica
publisher.none.fl_str_mv Instituto Tecnológico de Aeronáutica
dc.source.none.fl_str_mv reponame:Biblioteca Digital de Teses e Dissertações do ITA
instname:Instituto Tecnológico de Aeronáutica
instacron:ITA
reponame_str Biblioteca Digital de Teses e Dissertações do ITA
collection Biblioteca Digital de Teses e Dissertações do ITA
instname_str Instituto Tecnológico de Aeronáutica
instacron_str ITA
institution ITA
repository.name.fl_str_mv Biblioteca Digital de Teses e Dissertações do ITA - Instituto Tecnológico de Aeronáutica
repository.mail.fl_str_mv
subject_por_txtF_mv Atuadores
Controle de pilotagem por fios
Modelos matemáticos
Algoritmos genéticos
Controle automático de vôo
Projeto de aeronaves
Simulação computadorizada
Superfícies de controle
Engenharia aeronáutica
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