Analysis of Bifurcation Parameters by Metric Representation linearized of an Aeronautical System

Author

Carrillo, Jesus ; Reynoso, Gilberto ; Del Carmen Rodriguez, Guadalupe ; Garcia, Miguel Angel

Author_Institution

Univ. del Papaloapan, Tuxtepec, Mexico

Volume

13

Issue

7

fYear

2015

fDate

7/1/2015 12:00:00 AM

Firstpage

2065

Lastpage

2070

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.

Keywords

aerospace control; bifurcation; linearisation techniques; matrix algebra; nonlinear control systems; Taylor series expansion; aeronautical system; bifurcation parameters; first-order partial derivatives; linearized system; matrix elements; metric representation; nominal values; nonlinear system; second-order partial derivatives; Benchmark testing; Bifurcation; Current measurement; MIMO; Pollution measurement; Rotors; Transmission line measurements; Taylor series; aeronautic systems; linearization; nonlinear systems;

fLanguage

English

Journal_Title

Latin America Transactions, IEEE (Revista IEEE America Latina)

Publisher

ieee

ISSN

1548-0992

Type

jour

DOI

10.1109/TLA.2015.7273759

Filename

7273759