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'...

Ausführliche Beschreibung

Bibliographische Detailangaben
Hauptverfasser:	Higuera-Martínez, Oscar Iván, Salamanca, Juan Mauricio
Format:	Online
Sprache:	spa
Veröffentlicht:	Universidad Pedagógica y Tecnológica de Colombia - UPTC 2007
Schlagworte:	optimization robust control linear matrix inequatilities helicopter genetic algorithms optimización control robusto desigualdades matriciales lineales helicóptero algoritmos genéticos
Online Zugang:	https://revistas.uptc.edu.co/index.php/ingenieria_sogamoso/article/view/856

Beschreibung
Zusammenfassung:	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.