A best practices method for aircraft flight control law design.

Detalhes bibliográficos
Ano de defesa: 2008
Autor(a) principal: Lucas Rubiano de Souza Cruz
Orientador(a): Não Informado pela instituição
Banca de defesa: Não Informado pela instituição
Tipo de documento: Dissertação
Tipo de acesso: Acesso aberto
Idioma: eng
Instituição de defesa: Instituto Tecnológico de Aeronáutica
Programa de Pós-Graduação: Não Informado pela instituição
Departamento: Não Informado pela instituição
País: Não Informado pela instituição
Palavras-chave em Português:
Controle de aeronaves
Controle robusto
Modelos matemáticos
Simulação computadorizada
Teoria de controle
Mecânica de vôo
Controle
Engenharia aeronáutica
Link de acesso: http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=705
Resumo: This work develops a systematic design procedure for flight control laws design which allows: the use of best practices; compatibility with current fly-by-wire implementation; and integration with aircraft and systems design. Such procedure is based on a two-degree-of-freedom control structure, the first degree of freedom defining input to output characteristics and the second coping with disturbance rejection, noise rejection and robustness. The procedure uses a frequency domain based uncertainty description for treating robustness. A case study comprising a primary longitudinal flight control law design for a business aircraft is defined to evaluate the procedure. Results show the adequacy of the procedure: to coalesce many different requirements into simpler ones; evidence compromises between different requirements; design robust control laws given a set of reasonable requirements.
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network_name_str Biblioteca Digital de Teses e Dissertações do ITA
spelling A best practices method for aircraft flight control law design.Controle de aeronavesControle robustoModelos matemáticosSimulação computadorizadaTeoria de controleMecânica de vôoControleEngenharia aeronáuticaThis work develops a systematic design procedure for flight control laws design which allows: the use of best practices; compatibility with current fly-by-wire implementation; and integration with aircraft and systems design. Such procedure is based on a two-degree-of-freedom control structure, the first degree of freedom defining input to output characteristics and the second coping with disturbance rejection, noise rejection and robustness. The procedure uses a frequency domain based uncertainty description for treating robustness. A case study comprising a primary longitudinal flight control law design for a business aircraft is defined to evaluate the procedure. Results show the adequacy of the procedure: to coalesce many different requirements into simpler ones; evidence compromises between different requirements; design robust control laws given a set of reasonable requirements.Instituto Tecnológico de AeronáuticaKarl Heinz KienitzLucas Rubiano de Souza Cruz2008-10-09info:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/masterThesishttp://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=705reponame:Biblioteca Digital de Teses e Dissertações do ITAinstname:Instituto Tecnológico de Aeronáuticainstacron:ITAenginfo:eu-repo/semantics/openAccessapplication/pdf2019-02-02T14:01:55Zoai:agregador.ibict.br.BDTD_ITA:oai:ita.br:705http://oai.bdtd.ibict.br/requestopendoar:null2020-05-28 19:34:01.152Biblioteca Digital de Teses e Dissertações do ITA - Instituto Tecnológico de Aeronáuticatrue
dc.title.none.fl_str_mv A best practices method for aircraft flight control law design.
title A best practices method for aircraft flight control law design.
spellingShingle A best practices method for aircraft flight control law design.
Lucas Rubiano de Souza Cruz
Controle de aeronaves
Controle robusto
Modelos matemáticos
Simulação computadorizada
Teoria de controle
Mecânica de vôo
Controle
Engenharia aeronáutica
title_short A best practices method for aircraft flight control law design.
title_full A best practices method for aircraft flight control law design.
title_fullStr A best practices method for aircraft flight control law design.
title_full_unstemmed A best practices method for aircraft flight control law design.
title_sort A best practices method for aircraft flight control law design.
author Lucas Rubiano de Souza Cruz
author_facet Lucas Rubiano de Souza Cruz
author_role author
dc.contributor.none.fl_str_mv Karl Heinz Kienitz
dc.contributor.author.fl_str_mv Lucas Rubiano de Souza Cruz
dc.subject.por.fl_str_mv Controle de aeronaves
Controle robusto
Modelos matemáticos
Simulação computadorizada
Teoria de controle
Mecânica de vôo
Controle
Engenharia aeronáutica
topic Controle de aeronaves
Controle robusto
Modelos matemáticos
Simulação computadorizada
Teoria de controle
Mecânica de vôo
Controle
Engenharia aeronáutica
dc.description.none.fl_txt_mv This work develops a systematic design procedure for flight control laws design which allows: the use of best practices; compatibility with current fly-by-wire implementation; and integration with aircraft and systems design. Such procedure is based on a two-degree-of-freedom control structure, the first degree of freedom defining input to output characteristics and the second coping with disturbance rejection, noise rejection and robustness. The procedure uses a frequency domain based uncertainty description for treating robustness. A case study comprising a primary longitudinal flight control law design for a business aircraft is defined to evaluate the procedure. Results show the adequacy of the procedure: to coalesce many different requirements into simpler ones; evidence compromises between different requirements; design robust control laws given a set of reasonable requirements.
description This work develops a systematic design procedure for flight control laws design which allows: the use of best practices; compatibility with current fly-by-wire implementation; and integration with aircraft and systems design. Such procedure is based on a two-degree-of-freedom control structure, the first degree of freedom defining input to output characteristics and the second coping with disturbance rejection, noise rejection and robustness. The procedure uses a frequency domain based uncertainty description for treating robustness. A case study comprising a primary longitudinal flight control law design for a business aircraft is defined to evaluate the procedure. Results show the adequacy of the procedure: to coalesce many different requirements into simpler ones; evidence compromises between different requirements; design robust control laws given a set of reasonable requirements.
publishDate 2008
dc.date.none.fl_str_mv 2008-10-09
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=705
url http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=705
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 aeronaves
Controle robusto
Modelos matemáticos
Simulação computadorizada
Teoria de controle
Mecânica de vôo
Controle
Engenharia aeronáutica
_version_ 1706804989348806656

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