Multifunctional missions for unmanned aircraft squadrons
Autor(a) principal: | |
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Data de Publicação: | 2015 |
Tipo de documento: | Tese |
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=3204 |
Resumo: | Typical applications, such as georeferencing, long travelings, and monitoring, can be executed by unmanned aircraft squadrons by assuming different formations, such as latitudinal and longitudinal formations and circular motion maintenance, respectively. In order that all these problems can be solved in one mission, the squadron must reconfigure itself among these different formations in an autonomous way. In this study it is proposed a multifunctional missions execution scheme for unmanned aircraft squadrons based on geometric formation reconfigurations. The problem is a multidisciplinary one, and addresses the following issues: A control strategy able to deal with the aircraft model nonlinearity; computational algorithms for reconfiguring the squadrons among its different formations, whose efficiency is not critical for real-time applications; a theoretical treatment that allows the proof of convergence among the several squadron formation reconfigurations, and an approach that contributes to the system robustness with regard to parametric uncertainties of the aircraft dynamic model. Solutions are presented for the sub-problems and it is proposed their integration for getting a scheme for running a multifunctional missions queue. |
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Multifunctional missions for unmanned aircraft squadronsControle automático de vooAeronave não-tripuladaAlgoritmosOtimização de projeto multidisciplinarPlanejamento de missãoNavegação autônomaControleEngenharia aeronáuticaTypical applications, such as georeferencing, long travelings, and monitoring, can be executed by unmanned aircraft squadrons by assuming different formations, such as latitudinal and longitudinal formations and circular motion maintenance, respectively. In order that all these problems can be solved in one mission, the squadron must reconfigure itself among these different formations in an autonomous way. In this study it is proposed a multifunctional missions execution scheme for unmanned aircraft squadrons based on geometric formation reconfigurations. The problem is a multidisciplinary one, and addresses the following issues: A control strategy able to deal with the aircraft model nonlinearity; computational algorithms for reconfiguring the squadrons among its different formations, whose efficiency is not critical for real-time applications; a theoretical treatment that allows the proof of convergence among the several squadron formation reconfigurations, and an approach that contributes to the system robustness with regard to parametric uncertainties of the aircraft dynamic model. Solutions are presented for the sub-problems and it is proposed their integration for getting a scheme for running a multifunctional missions queue.Instituto Tecnológico de AeronáuticaElder Moreira HemerlyPaulo André Sperandio Giacomin2015-02-20info:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/doctoralThesishttp://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=3204reponame:Biblioteca Digital de Teses e Dissertações do ITAinstname:Instituto Tecnológico de Aeronáuticainstacron:ITAenginfo:eu-repo/semantics/openAccessapplication/pdf2019-02-02T14:05:06Zoai:agregador.ibict.br.BDTD_ITA:oai:ita.br:3204http://oai.bdtd.ibict.br/requestopendoar:null2020-05-28 19:41:22.216Biblioteca Digital de Teses e Dissertações do ITA - Instituto Tecnológico de Aeronáuticatrue |
dc.title.none.fl_str_mv |
Multifunctional missions for unmanned aircraft squadrons |
title |
Multifunctional missions for unmanned aircraft squadrons |
spellingShingle |
Multifunctional missions for unmanned aircraft squadrons Paulo André Sperandio Giacomin Controle automático de voo Aeronave não-tripulada Algoritmos Otimização de projeto multidisciplinar Planejamento de missão Navegação autônoma Controle Engenharia aeronáutica |
title_short |
Multifunctional missions for unmanned aircraft squadrons |
title_full |
Multifunctional missions for unmanned aircraft squadrons |
title_fullStr |
Multifunctional missions for unmanned aircraft squadrons |
title_full_unstemmed |
Multifunctional missions for unmanned aircraft squadrons |
title_sort |
Multifunctional missions for unmanned aircraft squadrons |
author |
Paulo André Sperandio Giacomin |
author_facet |
Paulo André Sperandio Giacomin |
author_role |
author |
dc.contributor.none.fl_str_mv |
Elder Moreira Hemerly |
dc.contributor.author.fl_str_mv |
Paulo André Sperandio Giacomin |
dc.subject.por.fl_str_mv |
Controle automático de voo Aeronave não-tripulada Algoritmos Otimização de projeto multidisciplinar Planejamento de missão Navegação autônoma Controle Engenharia aeronáutica |
topic |
Controle automático de voo Aeronave não-tripulada Algoritmos Otimização de projeto multidisciplinar Planejamento de missão Navegação autônoma Controle Engenharia aeronáutica |
dc.description.none.fl_txt_mv |
Typical applications, such as georeferencing, long travelings, and monitoring, can be executed by unmanned aircraft squadrons by assuming different formations, such as latitudinal and longitudinal formations and circular motion maintenance, respectively. In order that all these problems can be solved in one mission, the squadron must reconfigure itself among these different formations in an autonomous way. In this study it is proposed a multifunctional missions execution scheme for unmanned aircraft squadrons based on geometric formation reconfigurations. The problem is a multidisciplinary one, and addresses the following issues: A control strategy able to deal with the aircraft model nonlinearity; computational algorithms for reconfiguring the squadrons among its different formations, whose efficiency is not critical for real-time applications; a theoretical treatment that allows the proof of convergence among the several squadron formation reconfigurations, and an approach that contributes to the system robustness with regard to parametric uncertainties of the aircraft dynamic model. Solutions are presented for the sub-problems and it is proposed their integration for getting a scheme for running a multifunctional missions queue. |
description |
Typical applications, such as georeferencing, long travelings, and monitoring, can be executed by unmanned aircraft squadrons by assuming different formations, such as latitudinal and longitudinal formations and circular motion maintenance, respectively. In order that all these problems can be solved in one mission, the squadron must reconfigure itself among these different formations in an autonomous way. In this study it is proposed a multifunctional missions execution scheme for unmanned aircraft squadrons based on geometric formation reconfigurations. The problem is a multidisciplinary one, and addresses the following issues: A control strategy able to deal with the aircraft model nonlinearity; computational algorithms for reconfiguring the squadrons among its different formations, whose efficiency is not critical for real-time applications; a theoretical treatment that allows the proof of convergence among the several squadron formation reconfigurations, and an approach that contributes to the system robustness with regard to parametric uncertainties of the aircraft dynamic model. Solutions are presented for the sub-problems and it is proposed their integration for getting a scheme for running a multifunctional missions queue. |
publishDate |
2015 |
dc.date.none.fl_str_mv |
2015-02-20 |
dc.type.driver.fl_str_mv |
info:eu-repo/semantics/publishedVersion info:eu-repo/semantics/doctoralThesis |
status_str |
publishedVersion |
format |
doctoralThesis |
dc.identifier.uri.fl_str_mv |
http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=3204 |
url |
http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=3204 |
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 automático de voo Aeronave não-tripulada Algoritmos Otimização de projeto multidisciplinar Planejamento de missão Navegação autônoma Controle Engenharia aeronáutica |
_version_ |
1706809296885383168 |