Bifurcation analysis of landing gear shimmy using flexible multibody models

Camiel J.J. Beckers; A. Emre Öngüt; Bert Verbeek; Rob H.B. Fey; Yves Lemmens; Nathan van de Wouw

Bifurcation analysis of landing gear shimmy using flexible multibody models

Camiel J.J. Beckers, A. Emre Öngüt, Bert Verbeek, Rob H.B. Fey, Yves Lemmens, Nathan van de Wouw

Dynamics and Control

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › Academic

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Abstract

Shimmy oscillations are undesired vibrations in aircraft landing gears. The onset of shimmy, marked by Hopf bifurcations, is investigated in the parameter space of an industrial, high-fidelity, flexible multibody landing gear model. The bifurcation analyses are performed by coupling the Virtual.Lab Motion multibody solver with the numerical continuation software AUTO. The resulting quasi-2-parameter bifurcation diagrams, involving aircraft velocity and vertical landing gear load, are verified using conventional time-domain simulations and are shown to guarantee significantly higher solution accuracy at a similar computational cost.

Original language	English
Title of host publication	Proceedings of the 5th Joint Conference on Multibody System Dynamics, Lisboa, Portugal
Editors	Jorge A. C. Ambrósio
Chapter	11
Publication status	Published - 26 Jun 2018

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Beckers, C. J. J., Öngüt, A. E., Verbeek, B., Fey, R. H. B., Lemmens, Y., & van de Wouw, N. (2018). Bifurcation analysis of landing gear shimmy using flexible multibody models. In J. A. C. Ambrósio (Ed.), Proceedings of the 5th Joint Conference on Multibody System Dynamics, Lisboa, Portugal [46] http://imsd2018.tecnico.ulisboa.pt/Web_Abstracts_IMSD2018/pdf/WEB_PAPERS/IMSD2018_Full_Paper_46.pdf

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title = "Bifurcation analysis of landing gear shimmy using flexible multibody models",

abstract = "Shimmy oscillations are undesired vibrations in aircraft landing gears. The onset of shimmy, marked by Hopf bifurcations, is investigated in the parameter space of an industrial, high-fidelity, flexible multibody landing gear model. The bifurcation analyses are performed by coupling the Virtual.Lab Motion multibody solver with the numerical continuation software AUTO. The resulting quasi-2-parameter bifurcation diagrams, involving aircraft velocity and vertical landing gear load, are verified using conventional time-domain simulations and are shown to guarantee significantly higher solution accuracy at a similar computational cost.",

author = "Beckers, {Camiel J.J.} and {\"O}ng{\"u}t, {A. Emre} and Bert Verbeek and Fey, {Rob H.B.} and Yves Lemmens and {van de Wouw}, Nathan",

year = "2018",

month = jun,

day = "26",

language = "English",

editor = "Ambr{\'o}sio, {Jorge A. C.}",

booktitle = "Proceedings of the 5th Joint Conference on Multibody System Dynamics, Lisboa, Portugal",

}

Beckers, CJJ, Öngüt, AE, Verbeek, B, Fey, RHB, Lemmens, Y & van de Wouw, N 2018, Bifurcation analysis of landing gear shimmy using flexible multibody models. in JAC Ambrósio (ed.), Proceedings of the 5th Joint Conference on Multibody System Dynamics, Lisboa, Portugal., 46. <http://imsd2018.tecnico.ulisboa.pt/Web_Abstracts_IMSD2018/pdf/WEB_PAPERS/IMSD2018_Full_Paper_46.pdf>

Bifurcation analysis of landing gear shimmy using flexible multibody models. / Beckers, Camiel J.J.; Öngüt, A. Emre; Verbeek, Bert; Fey, Rob H.B.; Lemmens, Yves; van de Wouw, Nathan.

Proceedings of the 5th Joint Conference on Multibody System Dynamics, Lisboa, Portugal. ed. / Jorge A. C. Ambrósio. 2018. 46.

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › Academic

TY - GEN

T1 - Bifurcation analysis of landing gear shimmy using flexible multibody models

AU - Beckers, Camiel J.J.

AU - Öngüt, A. Emre

AU - Verbeek, Bert

AU - Fey, Rob H.B.

AU - Lemmens, Yves

AU - van de Wouw, Nathan

PY - 2018/6/26

Y1 - 2018/6/26

N2 - Shimmy oscillations are undesired vibrations in aircraft landing gears. The onset of shimmy, marked by Hopf bifurcations, is investigated in the parameter space of an industrial, high-fidelity, flexible multibody landing gear model. The bifurcation analyses are performed by coupling the Virtual.Lab Motion multibody solver with the numerical continuation software AUTO. The resulting quasi-2-parameter bifurcation diagrams, involving aircraft velocity and vertical landing gear load, are verified using conventional time-domain simulations and are shown to guarantee significantly higher solution accuracy at a similar computational cost.

AB - Shimmy oscillations are undesired vibrations in aircraft landing gears. The onset of shimmy, marked by Hopf bifurcations, is investigated in the parameter space of an industrial, high-fidelity, flexible multibody landing gear model. The bifurcation analyses are performed by coupling the Virtual.Lab Motion multibody solver with the numerical continuation software AUTO. The resulting quasi-2-parameter bifurcation diagrams, involving aircraft velocity and vertical landing gear load, are verified using conventional time-domain simulations and are shown to guarantee significantly higher solution accuracy at a similar computational cost.

M3 - Conference contribution

BT - Proceedings of the 5th Joint Conference on Multibody System Dynamics, Lisboa, Portugal

A2 - Ambrósio, Jorge A. C.

ER -

Bifurcation analysis of landing gear shimmy using flexible multibody models

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