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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Detalles Bibliográficos

Autores principales:	Higuera-Martínez, Oscar Iván, Salamanca, Juan Mauricio
Formato:	Online
Lenguaje:	spa
Publicado:	Universidad Pedagógica y Tecnológica de Colombia - UPTC 2015
Materias:	robust control linear matrix inequalities nominal model nonlinear systems. control robusto desigualdades matriciales lineales modelo nominal sistema no lineal
Acceso en línea:	https://revistas.uptc.edu.co/index.php/ingenieria_sogamoso/article/view/4250