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'...

詳細記述

書誌詳細
主要な著者: Higuera-Martínez, Oscar Iván, Salamanca, Juan Mauricio
フォーマット: Online
言語:spa
出版事項: Universidad Pedagógica y Tecnológica de Colombia - UPTC 2007
主題:
オンライン・アクセス:https://revistas.uptc.edu.co/index.php/ingenieria_sogamoso/article/view/856
その他の書誌記述
要約: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.