Flight Control Design Considerations for Multicopters Operating in Adverse Atmospheric Conditions
- Autores
- Zumarraga, Augusto José; Concia, Bernardo Martín; Puleston, Pablo Federico
- Año de publicación
- 2018
- Idioma
- inglés
- Tipo de recurso
- documento de conferencia
- Estado
- versión publicada
- Descripción
- There is abundant literature related to the automatic control of multicopters showing the application of various control techniques, generally oriented to attitude control. This is one of the functions required for position and trajectory control, and is of greater academic interest due to its non-linear nature. However, it is not common to explore the conflicts that arise in the design when seeking to achieve high precision position control in adverse weather conditions. In this paper we analyze objectives, structural limitations and implementation needs that significantly impact the performance of a control system under these conditions. Some design criteria are proposed and the aptitude of a linear control scheme is evaluated to respond to these requirements. The development efforts are also discussed to achieve the required precisions in the estimation of position for an application of these characteristics.
Facultad de Ingeniería
Instituto de Investigaciones en Electrónica, Control y Procesamiento de Señales - Materia
-
Ingeniería
multicopter
flight control
LQG
atmospheric perturbation
integrated navigation - Nivel de accesibilidad
- acceso abierto
- Condiciones de uso
- http://creativecommons.org/licenses/by-nc-sa/4.0/
- Repositorio
- Institución
- Universidad Nacional de La Plata
- OAI Identificador
- oai:sedici.unlp.edu.ar:10915/107602
Ver los metadatos del registro completo
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Flight Control Design Considerations for Multicopters Operating in Adverse Atmospheric ConditionsZumarraga, Augusto JoséConcia, Bernardo MartínPuleston, Pablo FedericoIngenieríamulticopterflight controlLQGatmospheric perturbationintegrated navigationThere is abundant literature related to the automatic control of multicopters showing the application of various control techniques, generally oriented to attitude control. This is one of the functions required for position and trajectory control, and is of greater academic interest due to its non-linear nature. However, it is not common to explore the conflicts that arise in the design when seeking to achieve high precision position control in adverse weather conditions. In this paper we analyze objectives, structural limitations and implementation needs that significantly impact the performance of a control system under these conditions. Some design criteria are proposed and the aptitude of a linear control scheme is evaluated to respond to these requirements. The development efforts are also discussed to achieve the required precisions in the estimation of position for an application of these characteristics.Facultad de IngenieríaInstituto de Investigaciones en Electrónica, Control y Procesamiento de Señales2018info:eu-repo/semantics/conferenceObjectinfo:eu-repo/semantics/publishedVersionObjeto de conferenciahttp://purl.org/coar/resource_type/c_5794info:ar-repo/semantics/documentoDeConferenciaapplication/pdfhttp://sedici.unlp.edu.ar/handle/10915/107602enginfo:eu-repo/semantics/altIdentifier/doi/10.23919/AADECA.2018.8577430info:eu-repo/semantics/openAccesshttp://creativecommons.org/licenses/by-nc-sa/4.0/Creative Commons Attribution-NonCommercial-ShareAlike 4.0 International (CC BY-NC-SA 4.0)reponame:SEDICI (UNLP)instname:Universidad Nacional de La Platainstacron:UNLP2025-09-29T11:24:06Zoai:sedici.unlp.edu.ar:10915/107602Institucionalhttp://sedici.unlp.edu.ar/Universidad públicaNo correspondehttp://sedici.unlp.edu.ar/oai/snrdalira@sedici.unlp.edu.arArgentinaNo correspondeNo correspondeNo correspondeopendoar:13292025-09-29 11:24:06.78SEDICI (UNLP) - Universidad Nacional de La Platafalse |
dc.title.none.fl_str_mv |
Flight Control Design Considerations for Multicopters Operating in Adverse Atmospheric Conditions |
title |
Flight Control Design Considerations for Multicopters Operating in Adverse Atmospheric Conditions |
spellingShingle |
Flight Control Design Considerations for Multicopters Operating in Adverse Atmospheric Conditions Zumarraga, Augusto José Ingeniería multicopter flight control LQG atmospheric perturbation integrated navigation |
title_short |
Flight Control Design Considerations for Multicopters Operating in Adverse Atmospheric Conditions |
title_full |
Flight Control Design Considerations for Multicopters Operating in Adverse Atmospheric Conditions |
title_fullStr |
Flight Control Design Considerations for Multicopters Operating in Adverse Atmospheric Conditions |
title_full_unstemmed |
Flight Control Design Considerations for Multicopters Operating in Adverse Atmospheric Conditions |
title_sort |
Flight Control Design Considerations for Multicopters Operating in Adverse Atmospheric Conditions |
dc.creator.none.fl_str_mv |
Zumarraga, Augusto José Concia, Bernardo Martín Puleston, Pablo Federico |
author |
Zumarraga, Augusto José |
author_facet |
Zumarraga, Augusto José Concia, Bernardo Martín Puleston, Pablo Federico |
author_role |
author |
author2 |
Concia, Bernardo Martín Puleston, Pablo Federico |
author2_role |
author author |
dc.subject.none.fl_str_mv |
Ingeniería multicopter flight control LQG atmospheric perturbation integrated navigation |
topic |
Ingeniería multicopter flight control LQG atmospheric perturbation integrated navigation |
dc.description.none.fl_txt_mv |
There is abundant literature related to the automatic control of multicopters showing the application of various control techniques, generally oriented to attitude control. This is one of the functions required for position and trajectory control, and is of greater academic interest due to its non-linear nature. However, it is not common to explore the conflicts that arise in the design when seeking to achieve high precision position control in adverse weather conditions. In this paper we analyze objectives, structural limitations and implementation needs that significantly impact the performance of a control system under these conditions. Some design criteria are proposed and the aptitude of a linear control scheme is evaluated to respond to these requirements. The development efforts are also discussed to achieve the required precisions in the estimation of position for an application of these characteristics. Facultad de Ingeniería Instituto de Investigaciones en Electrónica, Control y Procesamiento de Señales |
description |
There is abundant literature related to the automatic control of multicopters showing the application of various control techniques, generally oriented to attitude control. This is one of the functions required for position and trajectory control, and is of greater academic interest due to its non-linear nature. However, it is not common to explore the conflicts that arise in the design when seeking to achieve high precision position control in adverse weather conditions. In this paper we analyze objectives, structural limitations and implementation needs that significantly impact the performance of a control system under these conditions. Some design criteria are proposed and the aptitude of a linear control scheme is evaluated to respond to these requirements. The development efforts are also discussed to achieve the required precisions in the estimation of position for an application of these characteristics. |
publishDate |
2018 |
dc.date.none.fl_str_mv |
2018 |
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info:eu-repo/semantics/conferenceObject info:eu-repo/semantics/publishedVersion Objeto de conferencia http://purl.org/coar/resource_type/c_5794 info:ar-repo/semantics/documentoDeConferencia |
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http://sedici.unlp.edu.ar/handle/10915/107602 |
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eng |
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eng |
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info:eu-repo/semantics/altIdentifier/doi/10.23919/AADECA.2018.8577430 |
dc.rights.none.fl_str_mv |
info:eu-repo/semantics/openAccess http://creativecommons.org/licenses/by-nc-sa/4.0/ Creative Commons Attribution-NonCommercial-ShareAlike 4.0 International (CC BY-NC-SA 4.0) |
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openAccess |
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http://creativecommons.org/licenses/by-nc-sa/4.0/ Creative Commons Attribution-NonCommercial-ShareAlike 4.0 International (CC BY-NC-SA 4.0) |
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