Robust Controller LMI for helicopter with two degrees of freedom

This article presents the design of a robust H∞ controller using techniques of linear matrix inequalities (LMIs) for controlling the position of Pitch and Yaw in a helicopter. Designing a FF + LMI controller is presented for stabilizing the system, and further the design of LMI + FF + integrator con...

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 2015
主題:
オンライン・アクセス:https://revistas.uptc.edu.co/index.php/ingenieria_sogamoso/article/view/4250