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'...

Mô tả đầy đủ

Chi tiết về thư mục
Những tác giả chính:	Higuera-Martínez, Oscar Iván, Salamanca, Juan Mauricio
Định dạng:	Online
Ngôn ngữ:	spa
Được phát hành:	Universidad Pedagógica y Tecnológica de Colombia - UPTC 2007
Những chủ đề:	optimization robust control linear matrix inequatilities helicopter genetic algorithms optimización control robusto desigualdades matriciales lineales helicóptero algoritmos genéticos
Truy cập trực tuyến:	https://revistas.uptc.edu.co/index.php/ingenieria_sogamoso/article/view/856

Miêu tả
Tóm tắt:	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.