Canonical description of the control system in the shimmy problem for the landing gear wheels of an aircraft

DOI10.1007/S10778-011-0455-0zbMath1272.70134OpenAlexW2094343920MaRDI QIDQ366905

V. I. Goncharenko

Publication date: 25 September 2013

Published in: International Applied Mechanics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s10778-011-0455-0

zbMATH Keywords

control systemwheelscomplex dynamic stiffnesslanding gearshimmy

Mathematics Subject Classification ID

Control of mechanical systems (70Q05) Motion of a rigid body in contact with a solid surface (70E18)

Related Items (2)

Using nonlinear feedback control to improve aircraft nose landing gear shimmy performance ⋮ Bifurcations of the self-exciting oscillations of a wheeled assembly about straight-line motion

Cites Work

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