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Geometric nonlinearities of aircraft systems

    Research output: Working paper

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    Abstract

    Nonlinearities due to geometric effects, in particular, via angular variables that are not small, are important for aircraft operation. Geometric nonlinearities have a strong effect on the dynamics of the aircraft system under consideration, and they are especially pronounced in aircraft ground operations. As a concrete example we consider here the effect of a non-zero rake angle on the dynamics of a nose landing gear. More specifically, we use tools from bifurcation theory to investigate the stability of the straight-rolling motion during a take-off run.
    Original languageEnglish
    Publication statusPublished - Aug 2009

    Bibliographical note

    Sponsorship: This research has been supported by Airbus in the UK.

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      • 1 Conference Contribution (Conference Proceeding)

      • Geometric nonlinearities of aircraft systems

        Krauskopf, B., Thota, P. & Lowenberg, M., Jun 2008, European Consortium for Mathematics in Industry (ECMI) Mini-Symposium 27: Dynamical Systems Methods in Aerospace Engineering, London, UK.

        Research output: Chapter in Book/Report/Conference proceeding › Conference Contribution (Conference Proceeding)

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