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Algebraic analysis of stability and bifurcation for nonlinear flight dynamics

  • D. Wang*
  • *Corresponding author for this work
  • Laboratoire d'Informatique de Paris 6

Research output: Contribution to journalArticlepeer-review

Abstract

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.

Original languageEnglish
Pages (from-to)345-349
Number of pages5
JournalAeronautical Journal
Volume115
Issue number1168
DOIs
StatePublished - Jun 2011
Externally publishedYes

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