Trajectory tracking of a quadcopter with an attached payload mass under external disturbances
Autor(a) principal: | |
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Data de Publicação: | 2021 |
Outros Autores: | |
Tipo de documento: | Artigo de conferência |
Idioma: | eng |
Título da fonte: | Repositório Institucional da UNESP |
Texto Completo: | http://dx.doi.org/10.1109/INDUSCON51756.2021.9529651 http://hdl.handle.net/11449/222502 |
Resumo: | Unmanned Aerial Vehicles (UAVs) present the ability to carry different onboard systems, such as sensors, cameras, measurement tools. Especially under unexpected scenarios, such as the pandemic, the need for a cheap, fast and feasible solution makes the quadcopter a promising opportunity to overcome these challenges. Also, depending on the required mission, quadcopters ensures not only follow the desired trajectory but also guarantee the stability of their components. A robust controller is required to maintain the quadcopter in its initial path even under external disturbances as well as not inferring the quality of the measurement responses. In this context, the present article introduces the performance analysis of three controllers designed for a quadcopter carrying a payload under external disturbances. The results show that the second-order Sliding Mode Controller (SO-SMC) exhibits a more robust response against external disturbances and trajectory adherence in comparison to the First-Order SMC (FO-SMC) and Proportional Integral Derivative (PID). |
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Trajectory tracking of a quadcopter with an attached payload mass under external disturbancesExternal disturbanceSliding mode controlUnmanned aerial vechileUnmanned Aerial Vehicles (UAVs) present the ability to carry different onboard systems, such as sensors, cameras, measurement tools. Especially under unexpected scenarios, such as the pandemic, the need for a cheap, fast and feasible solution makes the quadcopter a promising opportunity to overcome these challenges. Also, depending on the required mission, quadcopters ensures not only follow the desired trajectory but also guarantee the stability of their components. A robust controller is required to maintain the quadcopter in its initial path even under external disturbances as well as not inferring the quality of the measurement responses. In this context, the present article introduces the performance analysis of three controllers designed for a quadcopter carrying a payload under external disturbances. The results show that the second-order Sliding Mode Controller (SO-SMC) exhibits a more robust response against external disturbances and trajectory adherence in comparison to the First-Order SMC (FO-SMC) and Proportional Integral Derivative (PID).Conselho Nacional de Desenvolvimento Científico e Tecnológico (CNPq)School of Engineering of Ilha Solteira São Paulo State University (UNESP), SPSchool of Engineering of Ilha Solteira São Paulo State University (UNESP), SPCNPq: 429963/2016-5Universidade Estadual Paulista (UNESP)Geronel, Renan Sanches [UNESP]Bueno, Douglas Domingues [UNESP]2022-04-28T19:45:09Z2022-04-28T19:45:09Z2021-08-15info:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/conferenceObject1288-1295http://dx.doi.org/10.1109/INDUSCON51756.2021.95296512021 14th IEEE International Conference on Industry Applications, INDUSCON 2021 - Proceedings, p. 1288-1295.http://hdl.handle.net/11449/22250210.1109/INDUSCON51756.2021.95296512-s2.0-85115855759Scopusreponame:Repositório Institucional da UNESPinstname:Universidade Estadual Paulista (UNESP)instacron:UNESPeng2021 14th IEEE International Conference on Industry Applications, INDUSCON 2021 - Proceedingsinfo:eu-repo/semantics/openAccess2022-04-28T19:45:09Zoai:repositorio.unesp.br:11449/222502Repositório InstitucionalPUBhttp://repositorio.unesp.br/oai/requestopendoar:29462024-08-05T17:22:41.447992Repositório Institucional da UNESP - Universidade Estadual Paulista (UNESP)false |
dc.title.none.fl_str_mv |
Trajectory tracking of a quadcopter with an attached payload mass under external disturbances |
title |
Trajectory tracking of a quadcopter with an attached payload mass under external disturbances |
spellingShingle |
Trajectory tracking of a quadcopter with an attached payload mass under external disturbances Geronel, Renan Sanches [UNESP] External disturbance Sliding mode control Unmanned aerial vechile |
title_short |
Trajectory tracking of a quadcopter with an attached payload mass under external disturbances |
title_full |
Trajectory tracking of a quadcopter with an attached payload mass under external disturbances |
title_fullStr |
Trajectory tracking of a quadcopter with an attached payload mass under external disturbances |
title_full_unstemmed |
Trajectory tracking of a quadcopter with an attached payload mass under external disturbances |
title_sort |
Trajectory tracking of a quadcopter with an attached payload mass under external disturbances |
author |
Geronel, Renan Sanches [UNESP] |
author_facet |
Geronel, Renan Sanches [UNESP] Bueno, Douglas Domingues [UNESP] |
author_role |
author |
author2 |
Bueno, Douglas Domingues [UNESP] |
author2_role |
author |
dc.contributor.none.fl_str_mv |
Universidade Estadual Paulista (UNESP) |
dc.contributor.author.fl_str_mv |
Geronel, Renan Sanches [UNESP] Bueno, Douglas Domingues [UNESP] |
dc.subject.por.fl_str_mv |
External disturbance Sliding mode control Unmanned aerial vechile |
topic |
External disturbance Sliding mode control Unmanned aerial vechile |
description |
Unmanned Aerial Vehicles (UAVs) present the ability to carry different onboard systems, such as sensors, cameras, measurement tools. Especially under unexpected scenarios, such as the pandemic, the need for a cheap, fast and feasible solution makes the quadcopter a promising opportunity to overcome these challenges. Also, depending on the required mission, quadcopters ensures not only follow the desired trajectory but also guarantee the stability of their components. A robust controller is required to maintain the quadcopter in its initial path even under external disturbances as well as not inferring the quality of the measurement responses. In this context, the present article introduces the performance analysis of three controllers designed for a quadcopter carrying a payload under external disturbances. The results show that the second-order Sliding Mode Controller (SO-SMC) exhibits a more robust response against external disturbances and trajectory adherence in comparison to the First-Order SMC (FO-SMC) and Proportional Integral Derivative (PID). |
publishDate |
2021 |
dc.date.none.fl_str_mv |
2021-08-15 2022-04-28T19:45:09Z 2022-04-28T19:45:09Z |
dc.type.status.fl_str_mv |
info:eu-repo/semantics/publishedVersion |
dc.type.driver.fl_str_mv |
info:eu-repo/semantics/conferenceObject |
format |
conferenceObject |
status_str |
publishedVersion |
dc.identifier.uri.fl_str_mv |
http://dx.doi.org/10.1109/INDUSCON51756.2021.9529651 2021 14th IEEE International Conference on Industry Applications, INDUSCON 2021 - Proceedings, p. 1288-1295. http://hdl.handle.net/11449/222502 10.1109/INDUSCON51756.2021.9529651 2-s2.0-85115855759 |
url |
http://dx.doi.org/10.1109/INDUSCON51756.2021.9529651 http://hdl.handle.net/11449/222502 |
identifier_str_mv |
2021 14th IEEE International Conference on Industry Applications, INDUSCON 2021 - Proceedings, p. 1288-1295. 10.1109/INDUSCON51756.2021.9529651 2-s2.0-85115855759 |
dc.language.iso.fl_str_mv |
eng |
language |
eng |
dc.relation.none.fl_str_mv |
2021 14th IEEE International Conference on Industry Applications, INDUSCON 2021 - Proceedings |
dc.rights.driver.fl_str_mv |
info:eu-repo/semantics/openAccess |
eu_rights_str_mv |
openAccess |
dc.format.none.fl_str_mv |
1288-1295 |
dc.source.none.fl_str_mv |
Scopus reponame:Repositório Institucional da UNESP instname:Universidade Estadual Paulista (UNESP) instacron:UNESP |
instname_str |
Universidade Estadual Paulista (UNESP) |
instacron_str |
UNESP |
institution |
UNESP |
reponame_str |
Repositório Institucional da UNESP |
collection |
Repositório Institucional da UNESP |
repository.name.fl_str_mv |
Repositório Institucional da UNESP - Universidade Estadual Paulista (UNESP) |
repository.mail.fl_str_mv |
|
_version_ |
1808128801920516096 |