Design of LMI+I controller based in optimization for two degree of Freedom Helicopter

Its presents the Genetic Algorithms' use for the design's  optimization of a Robust control H8 using lineal Matrix Inequalities' techniques,  to control pitch and  yaw's  position in a two degrees of freedom helicopter. The optimization is carried out when the pitch and  yaw'...

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Main Authors: Higuera-Martínez, Oscar Iván, Salamanca, Juan Mauricio
Format: Online
Language:spa
Published: Universidad Pedagógica y Tecnológica de Colombia - UPTC 2007
Subjects:
Online Access:https://revistas.uptc.edu.co/index.php/ingenieria_sogamoso/article/view/856
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author Higuera-Martínez, Oscar Iván
Salamanca, Juan Mauricio
author_facet Higuera-Martínez, Oscar Iván
Salamanca, Juan Mauricio
author_sort Higuera-Martínez, Oscar Iván
collection OJS
description Its presents the Genetic Algorithms' use for the design's  optimization of a Robust control H8 using lineal Matrix Inequalities' techniques,  to control pitch and  yaw's  position in a two degrees of freedom helicopter. The optimization is carried out when the pitch and  yaw's speed sensor, based on the energy consumption fails, the maximum peak and oscillation frequency of the system. The simulations'  results are presented on the non-linear model system. 
format Online
id oai:oai.revistas.uptc.edu.co:article-856
institution Revista Ingeniería, Investigación y Desarrollo
language spa
publishDate 2007
publisher Universidad Pedagógica y Tecnológica de Colombia - UPTC
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spelling oai:oai.revistas.uptc.edu.co:article-8562017-09-08T00:54:54Z Design of LMI+I controller based in optimization for two degree of Freedom Helicopter Diseño de un controlador LMI+I basado en optimización para un helicóptero de dos grados de libertad Higuera-Martínez, Oscar Iván Salamanca, Juan Mauricio optimization robust control linear matrix inequatilities helicopter genetic algorithms optimización control robusto desigualdades matriciales lineales helicóptero algoritmos genéticos Its presents the Genetic Algorithms' use for the design's  optimization of a Robust control H8 using lineal Matrix Inequalities' techniques,  to control pitch and  yaw's  position in a two degrees of freedom helicopter. The optimization is carried out when the pitch and  yaw's speed sensor, based on the energy consumption fails, the maximum peak and oscillation frequency of the system. The simulations'  results are presented on the non-linear model system.  Presenta la optimización utilizando algoritmos genéticos para  el  diseño  de  un  controlador  robusto  H8  usando técnicas  de  desigualdades  matriciales  lineales  para controlar  la  posición  de  cabeceo  y  dirección  en  un helicóptero de dos grados de libertad. La optimización se realiza cuando falla el sensor de velocidad de cabeceo y dirección, con base en la energía consumida, el máximo sobrepico y  la frecuencia de oscilación del sistema. Se presentan  los  resultados  de  las  simulaciones  sobre  el modelo no  lineal del  sistema. Universidad Pedagógica y Tecnológica de Colombia - UPTC 2007-12-03 info:eu-repo/semantics/article info:eu-repo/semantics/publishedVersion application/pdf https://revistas.uptc.edu.co/index.php/ingenieria_sogamoso/article/view/856 Ingeniería Investigación y Desarrollo; Vol. 5 No. 2: julio-diciembre de 2007; 22-28 Ingeniería Investigación y Desarrollo; Vol. 5 Núm. 2: julio-diciembre de 2007; 22-28 2422-4324 1900-771X spa https://revistas.uptc.edu.co/index.php/ingenieria_sogamoso/article/view/856/855 Derechos de autor 2007 Ingeniería Investigación y Desarrollo
spellingShingle optimization
robust control
linear matrix inequatilities
helicopter
genetic algorithms
optimización
control robusto
desigualdades matriciales lineales
helicóptero
algoritmos genéticos
Higuera-Martínez, Oscar Iván
Salamanca, Juan Mauricio
Design of LMI+I controller based in optimization for two degree of Freedom Helicopter
title Design of LMI+I controller based in optimization for two degree of Freedom Helicopter
title_alt Diseño de un controlador LMI+I basado en optimización para un helicóptero de dos grados de libertad
title_full Design of LMI+I controller based in optimization for two degree of Freedom Helicopter
title_fullStr Design of LMI+I controller based in optimization for two degree of Freedom Helicopter
title_full_unstemmed Design of LMI+I controller based in optimization for two degree of Freedom Helicopter
title_short Design of LMI+I controller based in optimization for two degree of Freedom Helicopter
title_sort design of lmi i controller based in optimization for two degree of freedom helicopter
topic optimization
robust control
linear matrix inequatilities
helicopter
genetic algorithms
optimización
control robusto
desigualdades matriciales lineales
helicóptero
algoritmos genéticos
topic_facet optimization
robust control
linear matrix inequatilities
helicopter
genetic algorithms
optimización
control robusto
desigualdades matriciales lineales
helicóptero
algoritmos genéticos
url https://revistas.uptc.edu.co/index.php/ingenieria_sogamoso/article/view/856
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