Estudio de las características estáticas y dinámicas de los actuadores Electromecánicos (EMA) con GUI de MATLAB

The element simulation process is nowadays one of the most important means to evaluate possible performances in the operation of almost any object, for this reason the finite element analysis (FEM) and the finite difference method (FDM) are important for find out the transient response results, for...

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Autores:
Cruz Parra, José Tito
Tipo de recurso:
Trabajo de grado de pregrado
Fecha de publicación:
2022
Institución:
Universidad Antonio Nariño
Repositorio:
Repositorio UAN
Idioma:
spa
OAI Identifier:
oai:repositorio.uan.edu.co:123456789/6918
Acceso en línea:
http://repositorio.uan.edu.co/handle/123456789/6918
Palabra clave:
EMA
sistemas dinámicos
análisis estático
EMA
dynamic systems
static analysis
Rights
openAccess
License
Attribution-NonCommercial-NoDerivatives 4.0 International (CC BY-NC-ND 4.0)
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repository_id_str
dc.title.es_ES.fl_str_mv Estudio de las características estáticas y dinámicas de los actuadores Electromecánicos (EMA) con GUI de MATLAB
title Estudio de las características estáticas y dinámicas de los actuadores Electromecánicos (EMA) con GUI de MATLAB
spellingShingle Estudio de las características estáticas y dinámicas de los actuadores Electromecánicos (EMA) con GUI de MATLAB
EMA
sistemas dinámicos
análisis estático
EMA
dynamic systems
static analysis
title_short Estudio de las características estáticas y dinámicas de los actuadores Electromecánicos (EMA) con GUI de MATLAB
title_full Estudio de las características estáticas y dinámicas de los actuadores Electromecánicos (EMA) con GUI de MATLAB
title_fullStr Estudio de las características estáticas y dinámicas de los actuadores Electromecánicos (EMA) con GUI de MATLAB
title_full_unstemmed Estudio de las características estáticas y dinámicas de los actuadores Electromecánicos (EMA) con GUI de MATLAB
title_sort Estudio de las características estáticas y dinámicas de los actuadores Electromecánicos (EMA) con GUI de MATLAB
dc.creator.fl_str_mv Cruz Parra, José Tito
dc.contributor.advisor.spa.fl_str_mv Cucaita Gómez, Alexander
dc.contributor.author.spa.fl_str_mv Cruz Parra, José Tito
dc.subject.es_ES.fl_str_mv EMA
sistemas dinámicos
análisis estático
topic EMA
sistemas dinámicos
análisis estático
EMA
dynamic systems
static analysis
dc.subject.keyword.es_ES.fl_str_mv EMA
dynamic systems
static analysis
description The element simulation process is nowadays one of the most important means to evaluate possible performances in the operation of almost any object, for this reason the finite element analysis (FEM) and the finite difference method (FDM) are important for find out the transient response results, for this purpose MATLAB-Simulink is used to design actuators such as electromagnetic valves.
publishDate 2022
dc.date.accessioned.none.fl_str_mv 2022-09-01T20:14:12Z
dc.date.available.none.fl_str_mv 2022-09-01T20:14:12Z
dc.date.issued.spa.fl_str_mv 2022-06-04
dc.type.spa.fl_str_mv Trabajo de grado (Pregrado y/o Especialización)
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dc.identifier.uri.none.fl_str_mv http://repositorio.uan.edu.co/handle/123456789/6918
dc.identifier.bibliographicCitation.spa.fl_str_mv Abdel-Fadil, R., Eid, A., & Abdel-Salam, M. (2015). Control and performance investigation of modern civil aircraft actuators using model predictive control.
AbdElhafez, A. A., & Forsyth, A. J. (2009). A review of more-electric aircraft. International Conference on Aerospace Sciences and Aviation Technology, 13(AEROSPACE SCIENCES & AVIATION TECHNOLOGY, ASAT-13, May 26–28, 2009), 1–13.
Alden, R. (2013). Flight demonstration, evaluation and proposed applications for various all electric flight control actuation system concepts. Aerospace Design Conference, 1171.
Beni, A. H., & Hoseini, S. M. (2015). Output feedback control of uncertain nonlinear systems with backlash using neural networks. Majlesi Journal of Mechatronic Systems, 4(1).
Bennouna, O., & Langlois, N. (2013). Modeling and simulation of electromechanical actuators for aircraft nacelles. 1–5. https://doi.org/10.1109/ISMA.2013.6547389
Budinger, M., Hospital, F., Liscouet, J., & Maré, J.-C. (2010). Model Based Methodologies for the Assessment of More Electric Flight Control Actuators. 10th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference, 9119.
Choi, Y. H., Jang, S. H., & Oh, J. H. (2013). Influencing Factors on Stick-Slip Behavior of a Ball Screw Driven Elevation Mechanism for MLRS. Applied Mechanics and Materials, 271–272, 958–968. https://doi.org/10.4028/www.scientific.net/AMM.271272.958
Cornelius, C. C., & Lawlor, S. P. (2006). Roller screw system. Google Patents.
Cowan, J. R., & Weir, R. A. (1993). Design and test of electromechanical actuators for thrust vector control. 27th Aerospace Mechanisms Symposium, 349–366.
Erhart, T. A. (1996). Linear actuator with feedback position sensor device. Google Patents.
dc.identifier.instname.spa.fl_str_mv instname:Universidad Antonio Nariño
dc.identifier.reponame.spa.fl_str_mv reponame:Repositorio Institucional UAN
dc.identifier.repourl.spa.fl_str_mv repourl:https://repositorio.uan.edu.co/
url http://repositorio.uan.edu.co/handle/123456789/6918
identifier_str_mv Abdel-Fadil, R., Eid, A., & Abdel-Salam, M. (2015). Control and performance investigation of modern civil aircraft actuators using model predictive control.
AbdElhafez, A. A., & Forsyth, A. J. (2009). A review of more-electric aircraft. International Conference on Aerospace Sciences and Aviation Technology, 13(AEROSPACE SCIENCES & AVIATION TECHNOLOGY, ASAT-13, May 26–28, 2009), 1–13.
Alden, R. (2013). Flight demonstration, evaluation and proposed applications for various all electric flight control actuation system concepts. Aerospace Design Conference, 1171.
Beni, A. H., & Hoseini, S. M. (2015). Output feedback control of uncertain nonlinear systems with backlash using neural networks. Majlesi Journal of Mechatronic Systems, 4(1).
Bennouna, O., & Langlois, N. (2013). Modeling and simulation of electromechanical actuators for aircraft nacelles. 1–5. https://doi.org/10.1109/ISMA.2013.6547389
Budinger, M., Hospital, F., Liscouet, J., & Maré, J.-C. (2010). Model Based Methodologies for the Assessment of More Electric Flight Control Actuators. 10th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference, 9119.
Choi, Y. H., Jang, S. H., & Oh, J. H. (2013). Influencing Factors on Stick-Slip Behavior of a Ball Screw Driven Elevation Mechanism for MLRS. Applied Mechanics and Materials, 271–272, 958–968. https://doi.org/10.4028/www.scientific.net/AMM.271272.958
Cornelius, C. C., & Lawlor, S. P. (2006). Roller screw system. Google Patents.
Cowan, J. R., & Weir, R. A. (1993). Design and test of electromechanical actuators for thrust vector control. 27th Aerospace Mechanisms Symposium, 349–366.
Erhart, T. A. (1996). Linear actuator with feedback position sensor device. Google Patents.
instname:Universidad Antonio Nariño
reponame:Repositorio Institucional UAN
repourl:https://repositorio.uan.edu.co/
dc.language.iso.spa.fl_str_mv spa
language spa
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eu_rights_str_mv openAccess
dc.publisher.spa.fl_str_mv Universidad Antonio Nariño
dc.publisher.program.spa.fl_str_mv Ingeniería Electromecánica
dc.publisher.faculty.spa.fl_str_mv Facultad de Ingeniería Mecánica, Electrónica y Biomédica
dc.publisher.campus.spa.fl_str_mv Villavicencio
institution Universidad Antonio Nariño
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spelling Attribution-NonCommercial-NoDerivatives 4.0 International (CC BY-NC-ND 4.0)Acceso abiertohttps://creativecommons.org/licenses/by-nc-nd/4.0/info:eu-repo/semantics/openAccesshttp://purl.org/coar/access_right/c_abf2Cucaita Gómez, AlexanderCruz Parra, José Tito211316286762022-09-01T20:14:12Z2022-09-01T20:14:12Z2022-06-04http://repositorio.uan.edu.co/handle/123456789/6918Abdel-Fadil, R., Eid, A., & Abdel-Salam, M. (2015). Control and performance investigation of modern civil aircraft actuators using model predictive control.AbdElhafez, A. A., & Forsyth, A. J. (2009). A review of more-electric aircraft. International Conference on Aerospace Sciences and Aviation Technology, 13(AEROSPACE SCIENCES & AVIATION TECHNOLOGY, ASAT-13, May 26–28, 2009), 1–13.Alden, R. (2013). Flight demonstration, evaluation and proposed applications for various all electric flight control actuation system concepts. Aerospace Design Conference, 1171.Beni, A. H., & Hoseini, S. M. (2015). Output feedback control of uncertain nonlinear systems with backlash using neural networks. Majlesi Journal of Mechatronic Systems, 4(1).Bennouna, O., & Langlois, N. (2013). Modeling and simulation of electromechanical actuators for aircraft nacelles. 1–5. https://doi.org/10.1109/ISMA.2013.6547389Budinger, M., Hospital, F., Liscouet, J., & Maré, J.-C. (2010). Model Based Methodologies for the Assessment of More Electric Flight Control Actuators. 10th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference, 9119.Choi, Y. H., Jang, S. H., & Oh, J. H. (2013). Influencing Factors on Stick-Slip Behavior of a Ball Screw Driven Elevation Mechanism for MLRS. Applied Mechanics and Materials, 271–272, 958–968. https://doi.org/10.4028/www.scientific.net/AMM.271272.958Cornelius, C. C., & Lawlor, S. P. (2006). Roller screw system. Google Patents.Cowan, J. R., & Weir, R. A. (1993). Design and test of electromechanical actuators for thrust vector control. 27th Aerospace Mechanisms Symposium, 349–366.Erhart, T. A. (1996). Linear actuator with feedback position sensor device. Google Patents.instname:Universidad Antonio Nariñoreponame:Repositorio Institucional UANrepourl:https://repositorio.uan.edu.co/The element simulation process is nowadays one of the most important means to evaluate possible performances in the operation of almost any object, for this reason the finite element analysis (FEM) and the finite difference method (FDM) are important for find out the transient response results, for this purpose MATLAB-Simulink is used to design actuators such as electromagnetic valves.El proceso de simulación de elementos es hoy en día uno de los medios más importantes para evaluar desempeños posibles en el funcionamiento de casi cualquier objeto, por ello el análisis de elementos finitos (FEM) y el método de diferencias finitas (FDM) son importantes para averiguar los resultados de respuesta transitoria, para ello se usa MATLAB-Simulink para diseñar actuadores como válvulas electromagnéticas.Ingeniero(a) Electromecánico(a)PregradoDistanciaProyectospaUniversidad Antonio NariñoIngeniería ElectromecánicaFacultad de Ingeniería Mecánica, Electrónica y BiomédicaVillavicencioEMAsistemas dinámicosanálisis estáticoEMAdynamic systemsstatic analysisEstudio de las características estáticas y dinámicas de los actuadores Electromecánicos (EMA) con GUI de MATLABTrabajo de grado (Pregrado y/o Especialización)http://purl.org/coar/resource_type/c_7a1fhttp://purl.org/coar/version/c_970fb48d4fbd8a85EspecializadaORIGINAL2022_JoséTitoCruzParra2022_JoséTitoCruzParraRev. turnitinapplication/pdf1829098https://repositorio.uan.edu.co/bitstreams/31dfafb2-ffa6-42da-9e38-d49d0a00715d/downloadc4238261218a281bf6ca7d8eac39d348MD512022_JoséTitoCruzParra2022_JoséTitoCruzParraTrabajo finalapplication/pdf7147543https://repositorio.uan.edu.co/bitstreams/47072232-4193-4bd6-8d90-01b2f694c1a8/downloadbec7db1541e0568def3c9ed1ccb4ebd8MD522022_JoséTitoCruzParra_Autorización.pdf2022_JoséTitoCruzParra_Autorización.pdfAutorización de autoresapplication/pdf543034https://repositorio.uan.edu.co/bitstreams/39a3ad40-1ce5-4b4f-ad61-7e130f60dbb1/downloada9d1ff18b89d2671686eb7a7cb46b16bMD532022_JoséTitoCruzParra_Acta2022_JoséTitoCruzParra_ActaActa de sustentaciónapplication/pdf654822https://repositorio.uan.edu.co/bitstreams/47a449a4-ac57-4724-8d95-96f4b7fe0873/download2f335182cd77ecc9a24e155608e75db7MD54CC-LICENSElicense_rdflicense_rdfapplication/rdf+xml; charset=utf-8811https://repositorio.uan.edu.co/bitstreams/1dcc33b5-ab37-44a5-a138-081aae89b358/download9868ccc48a14c8d591352b6eaf7f6239MD55123456789/6918oai:repositorio.uan.edu.co:123456789/69182024-10-09 23:03:09.398https://creativecommons.org/licenses/by-nc-nd/4.0/Acceso abiertoopen.accesshttps://repositorio.uan.edu.coRepositorio Institucional UANalertas.repositorio@uan.edu.co

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