Interaction of torsion and lateral bending in aircraft nose landing gear shimmy

DOI10.1007/S11071-008-9455-YzbMath1176.74091OpenAlexW1968309189MaRDI QIDQ1041883

Phanikrishna Thota, Bernd Krauskopf, Mark Lowenberg

Publication date: 4 December 2009

Published in: Nonlinear Dynamics (Search for Journal in Brave)

Full work available at URL: https://research.vu.nl/ws/files/2490295/224287.pdf

zbMATH Keywords

quasiperiodic motionmode interactionshimmy oscillationsaircraft dynamics

Mathematics Subject Classification ID

Stability of dynamical problems in solid mechanics (74H55) Dynamical bifurcation of solutions to dynamical problems in solid mechanics (74H60)

Related Items (10)

Contact patch memory of tyres leading to lateral vibrations of four-wheeled vehicles ⋮ Using nonlinear feedback control to improve aircraft nose landing gear shimmy performance ⋮ Enhanced vehicle shimmy performance using inerter-based suppression mechanism ⋮ Unlocking a nose landing gear in different flight conditions: folds, cusps and a swallowtail ⋮ Discussion on: ``State feedback fuzzy adaptive control for active shimmy damping ⋮ Nonlinear energy sink to enhance the landing gear shimmy performance ⋮ Geometric Nonlinearities of Aircraft Systems ⋮ Theoretical and experimental study on the nonlinear dynamics of wheel-shimmy ⋮ Bifurcation-Based Shimmy Analysis of Landing Gears Using Flexible Multibody Models ⋮ Interaction of torsion and lateral bending in aircraft nose landing gear shimmy

Cites Work

• Unnamed Item
• Interaction of torsion and lateral bending in aircraft nose landing gear shimmy
• Nonlinear oscillations, dynamical systems, and bifurcations of vector fields
• NUMERICAL ANALYSIS AND CONTROL OF BIFURCATION PROBLEMS (II): BIFURCATION IN INFINITE DIMENSIONS
• Elements of applied bifurcation theory

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