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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Bibliografische gegevens
Hoofdauteurs:	Higuera-Martínez, Oscar Iván, Salamanca, Juan Mauricio
Formaat:	Online
Taal:	spa
Gepubliceerd in:	Universidad Pedagógica y Tecnológica de Colombia - UPTC 2007
Onderwerpen:	optimization robust control linear matrix inequatilities helicopter genetic algorithms optimización control robusto desigualdades matriciales lineales helicóptero algoritmos genéticos
Online toegang:	https://revistas.uptc.edu.co/index.php/ingenieria_sogamoso/article/view/856

Omschrijving
Samenvatting:	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.