Robust Controller LMI for helicopter with two degrees of freedom

This article presents the design of a robust H∞ controller using techniques of linear matrix inequalities (LMIs) for controlling the position of Pitch and Yaw in a helicopter. Designing a FF + LMI controller is presented for stabilizing the system, and further the design of LMI + FF + integrator con...

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Main Authors: Oscar Iván Higuera-Martínez, Juan Mauricio Salamanca
Format: Article
Language:Spanish
Published: Universidad Pedagógica y Tecnológica de Colombia 2015-06-01
Series:Ingeniería Investigación y Desarrollo
Subjects:
Online Access:http://revistas.uptc.edu.co/revistas/index.php/ingenieria_sogamoso/article/view/4250
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author Oscar Iván Higuera-Martínez
Juan Mauricio Salamanca
author_facet Oscar Iván Higuera-Martínez
Juan Mauricio Salamanca
author_sort Oscar Iván Higuera-Martínez
collection DOAJ
description This article presents the design of a robust H∞ controller using techniques of linear matrix inequalities (LMIs) for controlling the position of Pitch and Yaw in a helicopter. Designing a FF + LMI controller is presented for stabilizing the system, and further the design of LMI + FF + integrator controller is performed to make the tracking error equal to zero. Thereafter the results of simulations are showed on the nonlinear system model and a comparison with FF+LQR and FF+LQR+I which were developed by device manufacturers.
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last_indexed 2024-04-12T16:26:56Z
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spelling doaj.art-e50ca14b46774be59a41cbfbe04d07a22022-12-22T03:25:20ZspaUniversidad Pedagógica y Tecnológica de ColombiaIngeniería Investigación y Desarrollo1900-771X2422-43242015-06-01152475710.19053/1900771X.42503579Robust Controller LMI for helicopter with two degrees of freedomOscar Iván Higuera-Martínez0Juan Mauricio Salamanca1Universidad Pedagógica y Tecnológica de ColombiaUniversidad Pedagógica y Tecnológica de ColombiaThis article presents the design of a robust H∞ controller using techniques of linear matrix inequalities (LMIs) for controlling the position of Pitch and Yaw in a helicopter. Designing a FF + LMI controller is presented for stabilizing the system, and further the design of LMI + FF + integrator controller is performed to make the tracking error equal to zero. Thereafter the results of simulations are showed on the nonlinear system model and a comparison with FF+LQR and FF+LQR+I which were developed by device manufacturers.http://revistas.uptc.edu.co/revistas/index.php/ingenieria_sogamoso/article/view/4250control robustodesigualdades matriciales linealesmodelo nominalsistema no lineal
spellingShingle Oscar Iván Higuera-Martínez
Juan Mauricio Salamanca
Robust Controller LMI for helicopter with two degrees of freedom
Ingeniería Investigación y Desarrollo
control robusto
desigualdades matriciales lineales
modelo nominal
sistema no lineal
title Robust Controller LMI for helicopter with two degrees of freedom
title_full Robust Controller LMI for helicopter with two degrees of freedom
title_fullStr Robust Controller LMI for helicopter with two degrees of freedom
title_full_unstemmed Robust Controller LMI for helicopter with two degrees of freedom
title_short Robust Controller LMI for helicopter with two degrees of freedom
title_sort robust controller lmi for helicopter with two degrees of freedom
topic control robusto
desigualdades matriciales lineales
modelo nominal
sistema no lineal
url http://revistas.uptc.edu.co/revistas/index.php/ingenieria_sogamoso/article/view/4250
work_keys_str_mv AT oscarivanhigueramartinez robustcontrollerlmiforhelicopterwithtwodegreesoffreedom
AT juanmauriciosalamanca robustcontrollerlmiforhelicopterwithtwodegreesoffreedom