Análisis de los Parámetros de Bifurcación mediante la Métrica de Representación Linealizada de un Sistema Aeronáutico (Analysis of Bifurcation Parameters by Metric Representation linearized of an Aeronautical System)

Jesús Carrillo (jcarrillo@unpa.edu.mx)1, Gilberto Reynoso (g.reynosomeza@pucpr.br)2, Guadalupe del Carmen Rodríguez ( lupitarj@itver.edu.mx)3, Miguel Ángel García (miguelg@itver.edu.mx)3


1Universidad del Papaloapan
2Pontifícia Universidade Católica do Paraná (PUCPR)
3Instituto Tecnológico de Veracruz

This paper appears in: Revista IEEE América Latina

Publication Date: July 2015
Volume: 13,   Issue: 7 
ISSN: 1548-0992


Abstract:
A measurement of representation of a linearized system was used to determine the bifurcation parameters that may affect the linearization of a non-linear system as an aeronautical system. This measurement is based on the Taylor series expansion and was applied to aeronautic system. Current measurement considers that matrix elements resulting from left division of matrices containing second-order and first-order partial derivatives should be smaller than deviations from the nominal values

Index Terms:
nonlinear systems, linearization, Taylor series, aeronautic systems.   


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