Nonlinear adaptive control system for payload extraction operations
Autor(a) principal: | |
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Data de Publicação: | 2012 |
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=2239 |
Resumo: | This work covers the development of a nonlinear, adaptive control system for payload extraction operations. Load extractions are a critical type of maneuver which could make the longitudinal flight dynamics unstable. The online adaptation control strategy seems adequate for the problem, since it can deal with the drift in the plant parameters caused by the movement of the load inside the aircraft. The effects of a continuously varying C.G. position on the longitudinal flight dynamics are modeled in detail. The controller proposed consists on applying the technique of nonlinear inversion coupled with a model reference adaptive controller to deal with the unmodeled/unknown dynamics. The dynamic system considered for the control problem consists of the modeled aircraft dynamics augmented by the unknown parameters - whose dynamics are controlled by the chosen adaptation laws. The demonstration of stability for the complete system is done via Lyapunov';s stability theorem for nonlinear dynamic systems. A suitable Lyapunov Function Candidate used for such a demonstration is proposed in this work. Simulation results are presented and discussed based on the theory and on comparison with other control methods performance when applied to the same problem. |
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Biblioteca Digital de Teses e Dissertações do ITA |
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Nonlinear adaptive control system for payload extraction operationsControle de aeronavesSistemas não-linearesControle adaptativoAlijamento de cargasSimulação computadorizadaEngenharia mecânicaEngenharia aeronáuticaThis work covers the development of a nonlinear, adaptive control system for payload extraction operations. Load extractions are a critical type of maneuver which could make the longitudinal flight dynamics unstable. The online adaptation control strategy seems adequate for the problem, since it can deal with the drift in the plant parameters caused by the movement of the load inside the aircraft. The effects of a continuously varying C.G. position on the longitudinal flight dynamics are modeled in detail. The controller proposed consists on applying the technique of nonlinear inversion coupled with a model reference adaptive controller to deal with the unmodeled/unknown dynamics. The dynamic system considered for the control problem consists of the modeled aircraft dynamics augmented by the unknown parameters - whose dynamics are controlled by the chosen adaptation laws. The demonstration of stability for the complete system is done via Lyapunov';s stability theorem for nonlinear dynamic systems. A suitable Lyapunov Function Candidate used for such a demonstration is proposed in this work. Simulation results are presented and discussed based on the theory and on comparison with other control methods performance when applied to the same problem.Instituto Tecnológico de AeronáuticaPedro PaglioneGustavo Oliveira Violato2012-12-14info:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/masterThesishttp://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=2239reponame:Biblioteca Digital de Teses e Dissertações do ITAinstname:Instituto Tecnológico de Aeronáuticainstacron:ITAenginfo:eu-repo/semantics/openAccessapplication/pdf2019-02-02T14:04:44Zoai:agregador.ibict.br.BDTD_ITA:oai:ita.br:2239http://oai.bdtd.ibict.br/requestopendoar:null2020-05-28 19:38:36.391Biblioteca Digital de Teses e Dissertações do ITA - Instituto Tecnológico de Aeronáuticatrue |
dc.title.none.fl_str_mv |
Nonlinear adaptive control system for payload extraction operations |
title |
Nonlinear adaptive control system for payload extraction operations |
spellingShingle |
Nonlinear adaptive control system for payload extraction operations Gustavo Oliveira Violato Controle de aeronaves Sistemas não-lineares Controle adaptativo Alijamento de cargas Simulação computadorizada Engenharia mecânica Engenharia aeronáutica |
title_short |
Nonlinear adaptive control system for payload extraction operations |
title_full |
Nonlinear adaptive control system for payload extraction operations |
title_fullStr |
Nonlinear adaptive control system for payload extraction operations |
title_full_unstemmed |
Nonlinear adaptive control system for payload extraction operations |
title_sort |
Nonlinear adaptive control system for payload extraction operations |
author |
Gustavo Oliveira Violato |
author_facet |
Gustavo Oliveira Violato |
author_role |
author |
dc.contributor.none.fl_str_mv |
Pedro Paglione |
dc.contributor.author.fl_str_mv |
Gustavo Oliveira Violato |
dc.subject.por.fl_str_mv |
Controle de aeronaves Sistemas não-lineares Controle adaptativo Alijamento de cargas Simulação computadorizada Engenharia mecânica Engenharia aeronáutica |
topic |
Controle de aeronaves Sistemas não-lineares Controle adaptativo Alijamento de cargas Simulação computadorizada Engenharia mecânica Engenharia aeronáutica |
dc.description.none.fl_txt_mv |
This work covers the development of a nonlinear, adaptive control system for payload extraction operations. Load extractions are a critical type of maneuver which could make the longitudinal flight dynamics unstable. The online adaptation control strategy seems adequate for the problem, since it can deal with the drift in the plant parameters caused by the movement of the load inside the aircraft. The effects of a continuously varying C.G. position on the longitudinal flight dynamics are modeled in detail. The controller proposed consists on applying the technique of nonlinear inversion coupled with a model reference adaptive controller to deal with the unmodeled/unknown dynamics. The dynamic system considered for the control problem consists of the modeled aircraft dynamics augmented by the unknown parameters - whose dynamics are controlled by the chosen adaptation laws. The demonstration of stability for the complete system is done via Lyapunov';s stability theorem for nonlinear dynamic systems. A suitable Lyapunov Function Candidate used for such a demonstration is proposed in this work. Simulation results are presented and discussed based on the theory and on comparison with other control methods performance when applied to the same problem. |
description |
This work covers the development of a nonlinear, adaptive control system for payload extraction operations. Load extractions are a critical type of maneuver which could make the longitudinal flight dynamics unstable. The online adaptation control strategy seems adequate for the problem, since it can deal with the drift in the plant parameters caused by the movement of the load inside the aircraft. The effects of a continuously varying C.G. position on the longitudinal flight dynamics are modeled in detail. The controller proposed consists on applying the technique of nonlinear inversion coupled with a model reference adaptive controller to deal with the unmodeled/unknown dynamics. The dynamic system considered for the control problem consists of the modeled aircraft dynamics augmented by the unknown parameters - whose dynamics are controlled by the chosen adaptation laws. The demonstration of stability for the complete system is done via Lyapunov';s stability theorem for nonlinear dynamic systems. A suitable Lyapunov Function Candidate used for such a demonstration is proposed in this work. Simulation results are presented and discussed based on the theory and on comparison with other control methods performance when applied to the same problem. |
publishDate |
2012 |
dc.date.none.fl_str_mv |
2012-12-14 |
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=2239 |
url |
http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=2239 |
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 Sistemas não-lineares Controle adaptativo Alijamento de cargas Simulação computadorizada Engenharia mecânica Engenharia aeronáutica |
_version_ |
1706809281935835136 |