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...

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Bibliographic Details
Main Authors: Higuera-Martínez, Oscar Iván, Salamanca, Juan Mauricio
Format: Online
Language:spa
Published: Universidad Pedagógica y Tecnológica de Colombia - UPTC 2015
Subjects:
Online Access:https://revistas.uptc.edu.co/index.php/ingenieria_sogamoso/article/view/4250