Attribution-NonCommercial-NoDerivatives 4.0 International (CC BY-NC-ND 4.0)Cucaita Gómez, AlexanderCruz Parra, José Tito2022-09-012022-09-012022-06-04http://repositorio.uan.edu.co/handle/123456789/6918The 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.spaAcceso abiertoEMAsistemas dinámicosanálisis estáticoTrabajo de grado (Pregrado y/o Especialización)EMAdynamic systemsstatic analysisinfo:eu-repo/semantics/openAccesshttp://purl.org/coar/access_right/c_abf2Abdel-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/