L0 and L1 Guidance and Path-Following Control for Airborne Wind Energy Systems

Detalhes bibliográficos
Autor(a) principal: Manuel C. R. M. Fernandes
Data de Publicação: 2022
Outros Autores: Sérgio Vinha, Luís Tiago Paiva, Fernando A. C. C. Fontes
Tipo de documento: Artigo
Idioma: eng
Título da fonte: Repositório Científico de Acesso Aberto de Portugal (Repositórios Cientìficos)
Texto Completo: https://hdl.handle.net/10216/140052
Resumo: For an efficient and reliable operation of an Airborne Wind Energy System, it is widely accepted that the kite should follow a pre-defined optimized path. In this article, we address the problem of designing a trajectory controller so that such path is closely followed. The path-following controllers investigated are based on a well-known nonlinear guidance logic termed L1 and on a proposed modification of it, which we termed L0. We have developed and implemented both L0 and L1 controllers for an AWES. The two controllers have an easy implementation with an explicit expression for the control law based on the cross-track error, on the heading angle relative to the path, and on a single parameter L (L-0 or L-1, depending on each controller) that we are able to tune. The L0 controller has an even easier implementation since the explicit control law can be used without the need to switch controllers. Since the switching of controllers might jeopardize stability, the L-0 controller has an important theoretical advantage in being able to guarantee stability on a larger domain of attraction. The simulation study shows that both nonlinear guidance logic controllers exhibit appropriate performance when the L parameter is adequately tuned, with the L0 controller showing a better performance when measured in terms of the average cross-track error.
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spelling L0 and L1 Guidance and Path-Following Control for Airborne Wind Energy SystemsFor an efficient and reliable operation of an Airborne Wind Energy System, it is widely accepted that the kite should follow a pre-defined optimized path. In this article, we address the problem of designing a trajectory controller so that such path is closely followed. The path-following controllers investigated are based on a well-known nonlinear guidance logic termed L1 and on a proposed modification of it, which we termed L0. We have developed and implemented both L0 and L1 controllers for an AWES. The two controllers have an easy implementation with an explicit expression for the control law based on the cross-track error, on the heading angle relative to the path, and on a single parameter L (L-0 or L-1, depending on each controller) that we are able to tune. The L0 controller has an even easier implementation since the explicit control law can be used without the need to switch controllers. Since the switching of controllers might jeopardize stability, the L-0 controller has an important theoretical advantage in being able to guarantee stability on a larger domain of attraction. The simulation study shows that both nonlinear guidance logic controllers exhibit appropriate performance when the L parameter is adequately tuned, with the L0 controller showing a better performance when measured in terms of the average cross-track error.20222022-01-01T00:00:00Zinfo:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/articleapplication/pdfhttps://hdl.handle.net/10216/140052eng1996-107310.3390/en15041390Manuel C. R. M. FernandesSérgio VinhaLuís Tiago PaivaFernando A. C. C. Fontesinfo:eu-repo/semantics/openAccessreponame:Repositório Científico de Acesso Aberto de Portugal (Repositórios Cientìficos)instname:Agência para a Sociedade do Conhecimento (UMIC) - FCT - Sociedade da Informaçãoinstacron:RCAAP2023-11-29T14:04:58Zoai:repositorio-aberto.up.pt:10216/140052Portal AgregadorONGhttps://www.rcaap.pt/oai/openaireopendoar:71602024-03-19T23:54:19.063386Repositório Científico de Acesso Aberto de Portugal (Repositórios Cientìficos) - Agência para a Sociedade do Conhecimento (UMIC) - FCT - Sociedade da Informaçãofalse
dc.title.none.fl_str_mv L0 and L1 Guidance and Path-Following Control for Airborne Wind Energy Systems
title L0 and L1 Guidance and Path-Following Control for Airborne Wind Energy Systems
spellingShingle L0 and L1 Guidance and Path-Following Control for Airborne Wind Energy Systems
Manuel C. R. M. Fernandes
title_short L0 and L1 Guidance and Path-Following Control for Airborne Wind Energy Systems
title_full L0 and L1 Guidance and Path-Following Control for Airborne Wind Energy Systems
title_fullStr L0 and L1 Guidance and Path-Following Control for Airborne Wind Energy Systems
title_full_unstemmed L0 and L1 Guidance and Path-Following Control for Airborne Wind Energy Systems
title_sort L0 and L1 Guidance and Path-Following Control for Airborne Wind Energy Systems
author Manuel C. R. M. Fernandes
author_facet Manuel C. R. M. Fernandes
Sérgio Vinha
Luís Tiago Paiva
Fernando A. C. C. Fontes
author_role author
author2 Sérgio Vinha
Luís Tiago Paiva
Fernando A. C. C. Fontes
author2_role author
author
author
dc.contributor.author.fl_str_mv Manuel C. R. M. Fernandes
Sérgio Vinha
Luís Tiago Paiva
Fernando A. C. C. Fontes
description For an efficient and reliable operation of an Airborne Wind Energy System, it is widely accepted that the kite should follow a pre-defined optimized path. In this article, we address the problem of designing a trajectory controller so that such path is closely followed. The path-following controllers investigated are based on a well-known nonlinear guidance logic termed L1 and on a proposed modification of it, which we termed L0. We have developed and implemented both L0 and L1 controllers for an AWES. The two controllers have an easy implementation with an explicit expression for the control law based on the cross-track error, on the heading angle relative to the path, and on a single parameter L (L-0 or L-1, depending on each controller) that we are able to tune. The L0 controller has an even easier implementation since the explicit control law can be used without the need to switch controllers. Since the switching of controllers might jeopardize stability, the L-0 controller has an important theoretical advantage in being able to guarantee stability on a larger domain of attraction. The simulation study shows that both nonlinear guidance logic controllers exhibit appropriate performance when the L parameter is adequately tuned, with the L0 controller showing a better performance when measured in terms of the average cross-track error.
publishDate 2022
dc.date.none.fl_str_mv 2022
2022-01-01T00:00:00Z
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dc.identifier.uri.fl_str_mv https://hdl.handle.net/10216/140052
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dc.language.iso.fl_str_mv eng
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dc.relation.none.fl_str_mv 1996-1073
10.3390/en15041390
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