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...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Higuera-Martínez, Oscar Iván, Salamanca, Juan Mauricio
Format:	Online
Sprache:	spa
Veröffentlicht:	Universidad Pedagógica y Tecnológica de Colombia - UPTC 2015
Schlagworte:	robust control linear matrix inequalities nominal model nonlinear systems. control robusto desigualdades matriciales lineales modelo nominal sistema no lineal
Online Zugang:	https://revistas.uptc.edu.co/index.php/ingenieria_sogamoso/article/view/4250