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'...

Полное описание

Библиографические подробности
Главные авторы: Higuera-Martínez, Oscar Iván, Salamanca, Juan Mauricio
Формат: Online
Язык:spa
Опубликовано: Universidad Pedagógica y Tecnológica de Colombia - UPTC 2007
Предметы:
Online-ссылка:https://revistas.uptc.edu.co/index.php/ingenieria_sogamoso/article/view/856
Описание
Итог: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.