Analysis of electro-hydrostatic actuator in more electric aircraft.
Autor(a) principal: | |
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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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Biblioteca Digital de Teses e Dissertações do ITA |
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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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1706809263797567488 |