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'...
- Autores:
- Tipo de recurso:
- http://purl.org/coar/resource_type/c_6686
- Fecha de publicación:
- 2007
- Institución:
- Universidad Pedagógica y Tecnológica de Colombia
- Repositorio:
- RiUPTC: Repositorio Institucional UPTC
- Idioma:
- spa
- OAI Identifier:
- oai:repositorio.uptc.edu.co:001/12133
- Acceso en línea:
- https://revistas.uptc.edu.co/index.php/ingenieria_sogamoso/article/view/856
https://repositorio.uptc.edu.co/handle/001/12133
- Palabra clave:
- optimization
robust control
linear matrix inequatilities
helicopter
genetic algorithms
optimización
control robusto
desigualdades matriciales lineales
helicóptero
algoritmos genéticos
- Rights
- License
- Derechos de autor 2007 Ingeniería Investigación y Desarrollo
id |
REPOUPTC2_5ba1224d35af23f7e23b952b0761f1b9 |
---|---|
oai_identifier_str |
oai:repositorio.uptc.edu.co:001/12133 |
network_acronym_str |
REPOUPTC2 |
network_name_str |
RiUPTC: Repositorio Institucional UPTC |
repository_id_str |
|
spelling |
2007-12-032024-07-05T18:47:35Z2024-07-05T18:47:35Zhttps://revistas.uptc.edu.co/index.php/ingenieria_sogamoso/article/view/856https://repositorio.uptc.edu.co/handle/001/12133Its 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.application/pdfspaspaUniversidad Pedagógica y Tecnológica de Colombia - UPTChttps://revistas.uptc.edu.co/index.php/ingenieria_sogamoso/article/view/856/855Derechos de autor 2007 Ingeniería Investigación y Desarrollohttp://purl.org/coar/access_right/c_abf187http://purl.org/coar/access_right/c_abf2Ingeniería Investigación y Desarrollo; Vol. 5 No. 2: julio-diciembre de 2007; 22-28Ingeniería Investigación y Desarrollo; Vol. 5 Núm. 2: julio-diciembre de 2007; 22-282422-43241900-771Xoptimizationrobust controllinear matrix inequatilitieshelicoptergenetic algorithmsoptimizacióncontrol robustodesigualdades matriciales linealeshelicópteroalgoritmos genéticosDesign of LMI+I controller based in optimization for two degree of Freedom HelicopterDiseño de un controlador LMI+I basado en optimización para un helicóptero de dos grados de libertadinfo:eu-repo/semantics/articlehttp://purl.org/coar/resource_type/c_6686http://purl.org/coar/resource_type/c_2df8fbb1http://purl.org/coar/version/c_970fb48d4fbd8a270http://purl.org/coar/version/c_970fb48d4fbd8a85Higuera-Martínez, Oscar IvánSalamanca, Juan Mauricio001/12133oai:repositorio.uptc.edu.co:001/121332025-07-18 11:25:46.421metadata.onlyhttps://repositorio.uptc.edu.coRepositorio Institucional UPTCrepositorio.uptc@uptc.edu.co |
dc.title.en-US.fl_str_mv |
Design of LMI+I controller based in optimization for two degree of Freedom Helicopter |
dc.title.es-ES.fl_str_mv |
Diseño de un controlador LMI+I basado en optimización para un helicóptero de dos grados de libertad |
title |
Design of LMI+I controller based in optimization for two degree of Freedom Helicopter |
spellingShingle |
Design of LMI+I controller based in optimization for two degree of Freedom Helicopter optimization robust control linear matrix inequatilities helicopter genetic algorithms optimización control robusto desigualdades matriciales lineales helicóptero algoritmos genéticos |
title_short |
Design of LMI+I controller based in optimization for two degree of Freedom Helicopter |
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_sort |
Design of LMI+I controller based in optimization for two degree of Freedom Helicopter |
dc.subject.en-US.fl_str_mv |
optimization robust control linear matrix inequatilities helicopter genetic algorithms |
topic |
optimization robust control linear matrix inequatilities helicopter genetic algorithms optimización control robusto desigualdades matriciales lineales helicóptero algoritmos genéticos |
dc.subject.es-ES.fl_str_mv |
optimización control robusto desigualdades matriciales lineales helicóptero algoritmos genéticos |
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. |
publishDate |
2007 |
dc.date.accessioned.none.fl_str_mv |
2024-07-05T18:47:35Z |
dc.date.available.none.fl_str_mv |
2024-07-05T18:47:35Z |
dc.date.none.fl_str_mv |
2007-12-03 |
dc.type.none.fl_str_mv |
info:eu-repo/semantics/article |
dc.type.coar.fl_str_mv |
http://purl.org/coar/resource_type/c_2df8fbb1 |
dc.type.coarversion.fl_str_mv |
http://purl.org/coar/version/c_970fb48d4fbd8a85 |
dc.type.coar.spa.fl_str_mv |
http://purl.org/coar/resource_type/c_6686 |
dc.type.coarversion.spa.fl_str_mv |
http://purl.org/coar/version/c_970fb48d4fbd8a270 |
format |
http://purl.org/coar/resource_type/c_6686 |
dc.identifier.none.fl_str_mv |
https://revistas.uptc.edu.co/index.php/ingenieria_sogamoso/article/view/856 |
dc.identifier.uri.none.fl_str_mv |
https://repositorio.uptc.edu.co/handle/001/12133 |
url |
https://revistas.uptc.edu.co/index.php/ingenieria_sogamoso/article/view/856 https://repositorio.uptc.edu.co/handle/001/12133 |
dc.language.none.fl_str_mv |
spa |
dc.language.iso.none.fl_str_mv |
spa |
language |
spa |
dc.relation.none.fl_str_mv |
https://revistas.uptc.edu.co/index.php/ingenieria_sogamoso/article/view/856/855 |
dc.rights.es-ES.fl_str_mv |
Derechos de autor 2007 Ingeniería Investigación y Desarrollo |
dc.rights.coar.fl_str_mv |
http://purl.org/coar/access_right/c_abf2 |
dc.rights.coar.spa.fl_str_mv |
http://purl.org/coar/access_right/c_abf187 |
rights_invalid_str_mv |
Derechos de autor 2007 Ingeniería Investigación y Desarrollo http://purl.org/coar/access_right/c_abf187 http://purl.org/coar/access_right/c_abf2 |
dc.format.none.fl_str_mv |
application/pdf |
dc.publisher.es-ES.fl_str_mv |
Universidad Pedagógica y Tecnológica de Colombia - UPTC |
dc.source.en-US.fl_str_mv |
Ingeniería Investigación y Desarrollo; Vol. 5 No. 2: julio-diciembre de 2007; 22-28 |
dc.source.es-ES.fl_str_mv |
Ingeniería Investigación y Desarrollo; Vol. 5 Núm. 2: julio-diciembre de 2007; 22-28 |
dc.source.none.fl_str_mv |
2422-4324 1900-771X |
institution |
Universidad Pedagógica y Tecnológica de Colombia |
repository.name.fl_str_mv |
Repositorio Institucional UPTC |
repository.mail.fl_str_mv |
repositorio.uptc@uptc.edu.co |
_version_ |
1839633864212873216 |