QFT FOR THE DESIGN OF AN AIRCRAFT FLIGHT CONTROL

Santander, A. y Aranda Almansa, Joaquín . (2005) QFT FOR THE DESIGN OF AN AIRCRAFT FLIGHT CONTROL. IFAC


Título QFT FOR THE DESIGN OF AN AIRCRAFT FLIGHT CONTROL
Autor(es) Santander, A.
Aranda Almansa, Joaquín
Materia(s) Informática
Resumen Array
Palabras clave Control
Aircraft
MIMO
Nonlinear
Robust
Editor(es) IFAC 2005
Fecha 2005-01-01
Identificador SA2005
bibliuned:680
Publicado en la Revista IFAC
Idioma eng
Versión de la publicación publishedVersion
Tipo de recurso Article
Derechos de acceso y licencia http://creativecommons.org/licenses/by-nc-nd/4.0
info:eu-repo/semantics/openAccess
Tipo de acceso Acceso abierto
Notas adicionales Aircraft flight control has a multivariable and non linear nature that makes it suitable for a verification of control capability of different designs. QFT techniques have been thoroughly used during the last years to provide robust control designs while using classic theory of control. The QFT method is applied to the design of an aircraft flight control and the results, evaluated by means of an automated software, can be compared to results obtained with different methodology approaches.

 
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Creado: Fri, 16 Nov 2007, 15:48:56 CET