dor_id: 4149183

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510.0.#.a: Scopus, Directory of Open Access Journals (DOAJ); Sistema Regional de Información en Línea para Revistas Científicas de América Latina, el Caribe, España y Portugal (Latindex); Indice de Revistas Latinoamericanas en Ciencias (Periódica); La Red de Revistas Científicas de América Latina y el Caribe, España y Portugal (Redalyc); Consejo Nacional de Ciencia y Tecnología (CONACyT); Google Scholar Citation

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336.#.#.b: article

336.#.#.3: Artículo de Investigación

336.#.#.a: Artículo

351.#.#.6: https://jart.icat.unam.mx/index.php/jart

351.#.#.b: Journal of Applied Research and Technology

351.#.#.a: Artículos

harvesting_group: RevistasUNAM

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856.4.0.u: https://jart.icat.unam.mx/index.php/jart/article/view/1741/1022

100.1.#.a: Breganon, Ricardo; Alves, Uiliam Nelson Lendzion Tomaz; de Almeida, João Paulo Lima Silva; Ribeiro, Fernando Sabino Fonteque; Mendonça, Marcio; Palácios, Rodrigo Henrique Cunha; Montezuma, Marcio Aurelio Furtado

524.#.#.a: Breganon, Ricardo, et al. (2023). Model Identification and H∞ Control of an Aeropendulum. Journal of Applied Research and Technology; Vol. 21 Núm. 4, 2023; 526-534. Recuperado de https://repositorio.unam.mx/contenidos/4149183

245.1.0.a: Model Identification and H∞ Control of an Aeropendulum

502.#.#.c: Universidad Nacional Autónoma de México

561.1.#.a: Instituto de Ciencias Aplicadas y Tecnología, UNAM

264.#.0.c: 2023

264.#.1.c: 2023-08-31

653.#.#.a: Aeropendulum; Model Identification

506.1.#.a: La titularidad de los derechos patrimoniales de esta obra pertenece a las instituciones editoras. Su uso se rige por una licencia Creative Commons BY-NC-ND 4.0 Internacional, https://creativecommons.org/licenses/by-nc-nd/4.0/legalcode.es, para un uso diferente consultar al responsable jurídico del repositorio por medio del correo electrónico gabriel.ascanio@icat.unam.mx

884.#.#.k: https://jart.icat.unam.mx/index.php/jart/article/view/1741

001.#.#.#: 074.oai:ojs2.localhost:article/1741

041.#.7.h: eng

520.3.#.a: The aeropendulum is a nonlinear system that consists of a rod equipped with a motorized propeller at one of its ends and connected to a pivot at its other end. This pivot receives a torsional moment through the aerodynamic effects generated by the propeller thrust force. From a control point of view, the aeropendulum is a plant that imposes a significant complexity on the design of controllers. In view of that, this system can be used in didactic observations and real applications of control theory concepts. This work presents the model identification and control of an aeropendulum system prototype. The model has as control input the voltage applied to the motor that drives the propeller and the rod angle as system output, measured by an incremental encoder. The identification process was conducted using the ident function of the Matlab® software. Based on the obtained model, an controller was designed to stabilize the system around the operating point, maintaining the rod in a specific position. A square wave was used as a reference for the angular variation of the rod to verify the controller"s efficiency in tracking a required angular trajectory. Simulation and experimental tests were conducted to validate the obtained mathematical model and the controller design. The results confirmed that the considered methodology was satisfactory for the studied case.

773.1.#.t: Journal of Applied Research and Technology; Vol. 21 Núm. 4 (2023); 526-534

773.1.#.o: https://jart.icat.unam.mx/index.php/jart

022.#.#.a: ISSN electrónico: 2448-6736; ISSN: 1665-6423

310.#.#.a: Bimestral

300.#.#.a: Páginas: 526-534

264.#.1.b: Instituto de Ciencias Aplicadas y Tecnología, UNAM

doi: https://doi.org/10.22201/icat.24486736e.2023.21.4.1741

harvesting_date: 2023-11-08 13:10:00.0

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file_creator: Yolanda G.G.

file_name: 109f7af425ec24ed0fd07041623648f72ffdd2eccb6918a1f26a3d421e3332d7.pdf

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last_modified: 2024-03-19 14:00:00

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Artículo

Model Identification and H∞ Control of an Aeropendulum

Breganon, Ricardo; Alves, Uiliam Nelson Lendzion Tomaz; de Almeida, João Paulo Lima Silva; Ribeiro, Fernando Sabino Fonteque; Mendonça, Marcio; Palácios, Rodrigo Henrique Cunha; Montezuma, Marcio Aurelio Furtado

Instituto de Ciencias Aplicadas y Tecnología, UNAM, publicado en Journal of Applied Research and Technology, y cosechado de Revistas UNAM

Licencia de uso

Procedencia del contenido

Cita

Breganon, Ricardo, et al. (2023). Model Identification and H∞ Control of an Aeropendulum. Journal of Applied Research and Technology; Vol. 21 Núm. 4, 2023; 526-534. Recuperado de https://repositorio.unam.mx/contenidos/4149183

Descripción del recurso

Autor(es)
Breganon, Ricardo; Alves, Uiliam Nelson Lendzion Tomaz; de Almeida, João Paulo Lima Silva; Ribeiro, Fernando Sabino Fonteque; Mendonça, Marcio; Palácios, Rodrigo Henrique Cunha; Montezuma, Marcio Aurelio Furtado
Tipo
Artículo de Investigación
Área del conocimiento
Ingenierías
Título
Model Identification and H∞ Control of an Aeropendulum
Fecha
2023-08-31
Resumen
The aeropendulum is a nonlinear system that consists of a rod equipped with a motorized propeller at one of its ends and connected to a pivot at its other end. This pivot receives a torsional moment through the aerodynamic effects generated by the propeller thrust force. From a control point of view, the aeropendulum is a plant that imposes a significant complexity on the design of controllers. In view of that, this system can be used in didactic observations and real applications of control theory concepts. This work presents the model identification and control of an aeropendulum system prototype. The model has as control input the voltage applied to the motor that drives the propeller and the rod angle as system output, measured by an incremental encoder. The identification process was conducted using the ident function of the Matlab® software. Based on the obtained model, an controller was designed to stabilize the system around the operating point, maintaining the rod in a specific position. A square wave was used as a reference for the angular variation of the rod to verify the controller"s efficiency in tracking a required angular trajectory. Simulation and experimental tests were conducted to validate the obtained mathematical model and the controller design. The results confirmed that the considered methodology was satisfactory for the studied case.
Tema
Aeropendulum; Model Identification
Idioma
eng
ISSN
ISSN electrónico: 2448-6736; ISSN: 1665-6423

Enlaces