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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Format: | Article |
Language: | Spanish |
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Universidad Pedagógica y Tecnológica de Colombia
2015-06-01
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Series: | Ingeniería Investigación y Desarrollo |
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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. |
first_indexed | 2024-04-12T16:26:56Z |
format | Article |
id | doaj.art-e50ca14b46774be59a41cbfbe04d07a2 |
institution | Directory Open Access Journal |
issn | 1900-771X 2422-4324 |
language | Spanish |
last_indexed | 2024-04-12T16:26:56Z |
publishDate | 2015-06-01 |
publisher | Universidad Pedagógica y Tecnológica de Colombia |
record_format | Article |
series | Ingeniería Investigación y Desarrollo |
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 |