Hydraulic actuation system modeling: an analysis of high frequency modeling

Detalhes bibliográficos
Autor(a) principal: Carlos Augusto Constantino
Data de Publicação: 2010
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=1307
Resumo: The objective of this work was to develop a high fidelity model representative up to high frequencies of a Flight Control System with hydraulic actuation on active-active mode. The usage of a Fly-By-Wire architecture and hydraulic actuation system on active-active mode has brought new engineering challenges like the force-fight between actuators and its structure fatigue life consumption on normal and failure scenarios such as oscillatory mal-functions. Once that these failure modes can exist up to high frequencies, it makes necessary the development of a high fidelity model of a flight control system representative up to high frequencies. The model herein developed has a high fidelity model of an EHSV, hydraulic actuator, a position loop and the control surface, as well as other models complementary in order that it can be possible to analyze the whole system up to high frequencies. It was analyzed the performance of the model at step input response and frequency response, showing to be a model close to the expected response of a real system. Also it was analyzed the frequency response of its components showing to be a representative model up to high frequencies. Besides the performance analysis, it was studied the behavior on a oscillatory mal-function scenario, showing the expected level of structure load, as well as its fatigue life consumption, showing the need to monitor these types of failures.
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spelling Hydraulic actuation system modeling: an analysis of high frequency modelingControle de vooSistemas hidráulicos de aeronavesControle de pilotagem por fiosAtuadoresSuperfícies de controleModelos matemáticosSimulação computadorizadaEngenharia aeronáuticaThe objective of this work was to develop a high fidelity model representative up to high frequencies of a Flight Control System with hydraulic actuation on active-active mode. The usage of a Fly-By-Wire architecture and hydraulic actuation system on active-active mode has brought new engineering challenges like the force-fight between actuators and its structure fatigue life consumption on normal and failure scenarios such as oscillatory mal-functions. Once that these failure modes can exist up to high frequencies, it makes necessary the development of a high fidelity model of a flight control system representative up to high frequencies. The model herein developed has a high fidelity model of an EHSV, hydraulic actuator, a position loop and the control surface, as well as other models complementary in order that it can be possible to analyze the whole system up to high frequencies. It was analyzed the performance of the model at step input response and frequency response, showing to be a model close to the expected response of a real system. Also it was analyzed the frequency response of its components showing to be a representative model up to high frequencies. Besides the performance analysis, it was studied the behavior on a oscillatory mal-function scenario, showing the expected level of structure load, as well as its fatigue life consumption, showing the need to monitor these types of failures.Instituto Tecnológico de AeronáuticaLuiz Carlos Sandoval GóesFernando José de Oliveira MoreiraCarlos Augusto Constantino2010-04-28info:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/masterThesishttp://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=1307reponame:Biblioteca Digital de Teses e Dissertações do ITAinstname:Instituto Tecnológico de Aeronáuticainstacron:ITAenginfo:eu-repo/semantics/openAccessapplication/pdf2019-02-02T14:02:39Zoai:agregador.ibict.br.BDTD_ITA:oai:ita.br:1307http://oai.bdtd.ibict.br/requestopendoar:null2020-05-28 19:36:01.847Biblioteca Digital de Teses e Dissertações do ITA - Instituto Tecnológico de Aeronáuticatrue
dc.title.none.fl_str_mv Hydraulic actuation system modeling: an analysis of high frequency modeling
title Hydraulic actuation system modeling: an analysis of high frequency modeling
spellingShingle Hydraulic actuation system modeling: an analysis of high frequency modeling
Carlos Augusto Constantino
Controle de voo
Sistemas hidráulicos de aeronaves
Controle de pilotagem por fios
Atuadores
Superfícies de controle
Modelos matemáticos
Simulação computadorizada
Engenharia aeronáutica
title_short Hydraulic actuation system modeling: an analysis of high frequency modeling
title_full Hydraulic actuation system modeling: an analysis of high frequency modeling
title_fullStr Hydraulic actuation system modeling: an analysis of high frequency modeling
title_full_unstemmed Hydraulic actuation system modeling: an analysis of high frequency modeling
title_sort Hydraulic actuation system modeling: an analysis of high frequency modeling
author Carlos Augusto Constantino
author_facet Carlos Augusto Constantino
author_role author
dc.contributor.none.fl_str_mv Luiz Carlos Sandoval Góes
Fernando José de Oliveira Moreira
dc.contributor.author.fl_str_mv Carlos Augusto Constantino
dc.subject.por.fl_str_mv Controle de voo
Sistemas hidráulicos de aeronaves
Controle de pilotagem por fios
Atuadores
Superfícies de controle
Modelos matemáticos
Simulação computadorizada
Engenharia aeronáutica
topic Controle de voo
Sistemas hidráulicos de aeronaves
Controle de pilotagem por fios
Atuadores
Superfícies de controle
Modelos matemáticos
Simulação computadorizada
Engenharia aeronáutica
dc.description.none.fl_txt_mv The objective of this work was to develop a high fidelity model representative up to high frequencies of a Flight Control System with hydraulic actuation on active-active mode. The usage of a Fly-By-Wire architecture and hydraulic actuation system on active-active mode has brought new engineering challenges like the force-fight between actuators and its structure fatigue life consumption on normal and failure scenarios such as oscillatory mal-functions. Once that these failure modes can exist up to high frequencies, it makes necessary the development of a high fidelity model of a flight control system representative up to high frequencies. The model herein developed has a high fidelity model of an EHSV, hydraulic actuator, a position loop and the control surface, as well as other models complementary in order that it can be possible to analyze the whole system up to high frequencies. It was analyzed the performance of the model at step input response and frequency response, showing to be a model close to the expected response of a real system. Also it was analyzed the frequency response of its components showing to be a representative model up to high frequencies. Besides the performance analysis, it was studied the behavior on a oscillatory mal-function scenario, showing the expected level of structure load, as well as its fatigue life consumption, showing the need to monitor these types of failures.
description The objective of this work was to develop a high fidelity model representative up to high frequencies of a Flight Control System with hydraulic actuation on active-active mode. The usage of a Fly-By-Wire architecture and hydraulic actuation system on active-active mode has brought new engineering challenges like the force-fight between actuators and its structure fatigue life consumption on normal and failure scenarios such as oscillatory mal-functions. Once that these failure modes can exist up to high frequencies, it makes necessary the development of a high fidelity model of a flight control system representative up to high frequencies. The model herein developed has a high fidelity model of an EHSV, hydraulic actuator, a position loop and the control surface, as well as other models complementary in order that it can be possible to analyze the whole system up to high frequencies. It was analyzed the performance of the model at step input response and frequency response, showing to be a model close to the expected response of a real system. Also it was analyzed the frequency response of its components showing to be a representative model up to high frequencies. Besides the performance analysis, it was studied the behavior on a oscillatory mal-function scenario, showing the expected level of structure load, as well as its fatigue life consumption, showing the need to monitor these types of failures.
publishDate 2010
dc.date.none.fl_str_mv 2010-04-28
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=1307
url http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=1307
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 Controle de voo
Sistemas hidráulicos de aeronaves
Controle de pilotagem por fios
Atuadores
Superfícies de controle
Modelos matemáticos
Simulação computadorizada
Engenharia aeronáutica
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