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...

Повний опис

Бібліографічні деталі
Автори: Higuera-Martínez, Oscar Iván, Salamanca, Juan Mauricio
Формат: Online
Мова:spa
Опубліковано: Universidad Pedagógica y Tecnológica de Colombia - UPTC 2015
Предмети:
Онлайн доступ:https://revistas.uptc.edu.co/index.php/ingenieria_sogamoso/article/view/4250