A fly-by-wire rudder control system design using multiobjective optimization.
Autor(a) principal: | |
---|---|
Data de Publicação: | 2009 |
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=1212 |
Resumo: | This work aims to demonstrate an approach to design a fly-by-wire mobile surface control system for a commercial jet employing multiobjective optimization techniques. This approach consists on sizing a set of design parameters of the control system based on model simulation and response analysis coupled with optimization algorithms in a multiobjective design environment. An overview on control surface systems is presented, focusing on fly-by-wire. To provide the theoretical basis, a review on optimization theory and methods is presented, as well it is developed the system mathematical model. The system in focus is of electro-hydraulic actuation, where a controller acts on a servo valve, that commands an actuator for positioning control of an aircraft rudder. The design approach was to optimize a set of system components parameters, such as controller gains, servo valve and hydraulic actuator parameters, that result in adequate workloads and produce a system that meets the design requirements and is cost-effective. The model, to be simulated and analyzed, is implemented in MATLAB/Simulink, from where the system response characteristics are passed to the optimization environment. A multiobjective genetic algorithm is applied, and as a result from the optimization process we obtain a Pareto set, from where an optimal design is chosen for a detailed analysis. |
id |
ITA_56caa0324f3884061d49b54feb352d62 |
---|---|
oai_identifier_str |
oai:agregador.ibict.br.BDTD_ITA:oai:ita.br:1212 |
network_acronym_str |
ITA |
network_name_str |
Biblioteca Digital de Teses e Dissertações do ITA |
spelling |
A fly-by-wire rudder control system design using multiobjective optimization.Otimização de paretoSistemas hidráulicos de aeronavesControle de pilotagem por fiosSuperfícies de controleModelos matemáticosSimulação computadorizadaEngenharia aeronáuticaThis work aims to demonstrate an approach to design a fly-by-wire mobile surface control system for a commercial jet employing multiobjective optimization techniques. This approach consists on sizing a set of design parameters of the control system based on model simulation and response analysis coupled with optimization algorithms in a multiobjective design environment. An overview on control surface systems is presented, focusing on fly-by-wire. To provide the theoretical basis, a review on optimization theory and methods is presented, as well it is developed the system mathematical model. The system in focus is of electro-hydraulic actuation, where a controller acts on a servo valve, that commands an actuator for positioning control of an aircraft rudder. The design approach was to optimize a set of system components parameters, such as controller gains, servo valve and hydraulic actuator parameters, that result in adequate workloads and produce a system that meets the design requirements and is cost-effective. The model, to be simulated and analyzed, is implemented in MATLAB/Simulink, from where the system response characteristics are passed to the optimization environment. A multiobjective genetic algorithm is applied, and as a result from the optimization process we obtain a Pareto set, from where an optimal design is chosen for a detailed analysis.Instituto Tecnológico de AeronáuticaRoberto Garcia NegrãoAlberto Adade FilhoBernardo Reis Dreyer de Souza2009-03-20info:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/masterThesishttp://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=1212reponame:Biblioteca Digital de Teses e Dissertações do ITAinstname:Instituto Tecnológico de Aeronáuticainstacron:ITAenginfo:eu-repo/semantics/openAccessapplication/pdf2019-02-02T14:02:36Zoai:agregador.ibict.br.BDTD_ITA:oai:ita.br:1212http://oai.bdtd.ibict.br/requestopendoar:null2020-05-28 19:35:43.115Biblioteca Digital de Teses e Dissertações do ITA - Instituto Tecnológico de Aeronáuticatrue |
dc.title.none.fl_str_mv |
A fly-by-wire rudder control system design using multiobjective optimization. |
title |
A fly-by-wire rudder control system design using multiobjective optimization. |
spellingShingle |
A fly-by-wire rudder control system design using multiobjective optimization. Bernardo Reis Dreyer de Souza Otimização de pareto Sistemas hidráulicos de aeronaves Controle de pilotagem por fios Superfícies de controle Modelos matemáticos Simulação computadorizada Engenharia aeronáutica |
title_short |
A fly-by-wire rudder control system design using multiobjective optimization. |
title_full |
A fly-by-wire rudder control system design using multiobjective optimization. |
title_fullStr |
A fly-by-wire rudder control system design using multiobjective optimization. |
title_full_unstemmed |
A fly-by-wire rudder control system design using multiobjective optimization. |
title_sort |
A fly-by-wire rudder control system design using multiobjective optimization. |
author |
Bernardo Reis Dreyer de Souza |
author_facet |
Bernardo Reis Dreyer de Souza |
author_role |
author |
dc.contributor.none.fl_str_mv |
Roberto Garcia Negrão Alberto Adade Filho |
dc.contributor.author.fl_str_mv |
Bernardo Reis Dreyer de Souza |
dc.subject.por.fl_str_mv |
Otimização de pareto Sistemas hidráulicos de aeronaves Controle de pilotagem por fios Superfícies de controle Modelos matemáticos Simulação computadorizada Engenharia aeronáutica |
topic |
Otimização de pareto Sistemas hidráulicos de aeronaves Controle de pilotagem por fios Superfícies de controle Modelos matemáticos Simulação computadorizada Engenharia aeronáutica |
dc.description.none.fl_txt_mv |
This work aims to demonstrate an approach to design a fly-by-wire mobile surface control system for a commercial jet employing multiobjective optimization techniques. This approach consists on sizing a set of design parameters of the control system based on model simulation and response analysis coupled with optimization algorithms in a multiobjective design environment. An overview on control surface systems is presented, focusing on fly-by-wire. To provide the theoretical basis, a review on optimization theory and methods is presented, as well it is developed the system mathematical model. The system in focus is of electro-hydraulic actuation, where a controller acts on a servo valve, that commands an actuator for positioning control of an aircraft rudder. The design approach was to optimize a set of system components parameters, such as controller gains, servo valve and hydraulic actuator parameters, that result in adequate workloads and produce a system that meets the design requirements and is cost-effective. The model, to be simulated and analyzed, is implemented in MATLAB/Simulink, from where the system response characteristics are passed to the optimization environment. A multiobjective genetic algorithm is applied, and as a result from the optimization process we obtain a Pareto set, from where an optimal design is chosen for a detailed analysis. |
description |
This work aims to demonstrate an approach to design a fly-by-wire mobile surface control system for a commercial jet employing multiobjective optimization techniques. This approach consists on sizing a set of design parameters of the control system based on model simulation and response analysis coupled with optimization algorithms in a multiobjective design environment. An overview on control surface systems is presented, focusing on fly-by-wire. To provide the theoretical basis, a review on optimization theory and methods is presented, as well it is developed the system mathematical model. The system in focus is of electro-hydraulic actuation, where a controller acts on a servo valve, that commands an actuator for positioning control of an aircraft rudder. The design approach was to optimize a set of system components parameters, such as controller gains, servo valve and hydraulic actuator parameters, that result in adequate workloads and produce a system that meets the design requirements and is cost-effective. The model, to be simulated and analyzed, is implemented in MATLAB/Simulink, from where the system response characteristics are passed to the optimization environment. A multiobjective genetic algorithm is applied, and as a result from the optimization process we obtain a Pareto set, from where an optimal design is chosen for a detailed analysis. |
publishDate |
2009 |
dc.date.none.fl_str_mv |
2009-03-20 |
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=1212 |
url |
http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=1212 |
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 |
Otimização de pareto Sistemas hidráulicos de aeronaves Controle de pilotagem por fios Superfícies de controle Modelos matemáticos Simulação computadorizada Engenharia aeronáutica |
_version_ |
1706809267308199936 |