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

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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Dades bibliogràfiques
Autors principals: Higuera-Martínez, Oscar Iván, Salamanca, Juan Mauricio
Format: Online
Idioma:spa
Publicat: Universidad Pedagógica y Tecnológica de Colombia - UPTC 2007
Matèries:
optimization
robust control
linear matrix inequatilities
helicopter
genetic algorithms
optimización
control robusto
desigualdades matriciales lineales
helicóptero
algoritmos genéticos
Accés en línia:https://revistas.uptc.edu.co/index.php/ingenieria_sogamoso/article/view/856
Descripció
Sumari: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.