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Algebraic analysis of stability and bifurcation for nonlinear flight dynamics

Published online by Cambridge University Press:  27 January 2016

D. Wang
D. Wang*
Affiliation:
Laboratoire d’Informatique de Paris 6, Université Pierre et Marie Curie – CNRS, Paris, France
*
Dongming.Wang@lip6.fr
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Abstract

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This note presents an application of algebraic methods to derive exact conditions for certain nonlinear flight dynamical systems to exhibit stability and bifurcation. The roll-coupling flight model is taken as an example to show the feasibility of algebraic analysis. Some of the previous stability and bifurcation results obtained using numerical analysis for this model are confirmed.

Information

Type
Research Article
Information
The Aeronautical Journal , Volume 115 , Issue 1168 , June 2011, pp. 345 - 349
Copyright
Copyright © Royal Aeronautical Society 2011 

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