Non Linear Dynamic Inversion Technique

Aranda Almansa, Joaquín, Non Linear Dynamic Inversion Technique. GROUP FOR AERONAUTICAL RESEARCH AND TECHNOLOGY IN EUROPE, 2007 (book)

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Título Non Linear Dynamic Inversion Technique
Autor(es) Aranda Almansa, Joaquín
Materia(s) Informática
Resumen Over the last two decades or so, control researchers have begun to apply alternative methodologies to flight control design. One alternative is variously called non-linear dynamic inversion or feedback linearization. The purpose of dynamic inversion is to develop a feedback control law that linearizes the plant response to commands. Simple controllers can then be designed. With dynamic inversion, a non-linear control law is designed which globally reduces the dynamics of selected controlled variables to integrators. A closed loop system is then designed to make the controlled variables exhibit specified command responses while satisfying the usual disturbances response and robustness requirements for the overall system and the various physical limitations of the aircraft’s control effectors.
Palabras clave ROBUST
CONTROL
TECHNIQUES
Non Linear
Dynamic
Inversion
Technique
Editor(es) GROUP FOR AERONAUTICAL RESEARCH AND TECHNOLOGY IN EUROPE
Fecha 2007-11-12
Identificador bibliuned:592
A97
http://e-spacio.uned.es/fez/view/bibliuned:592
Fuente ROBUST CONTROL TECHNIQUES
Idioma eng
Versión de la publicación publishedVersion
Nivel de acceso y licencia http://creativecommons.org/licenses/by-nc-nd/4.0
info:eu-repo/semantics/openAccess
Tipo de recurso book

 
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Creado: Mon, 12 Nov 2007, 13:36:26 CET