Pages that link to "Item:Q366905"
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The following pages link to Canonical description of the control system in the shimmy problem for the landing gear wheels of an aircraft (Q366905):
Displaying 4 items.
- State feedback fuzzy adaptive control for active shimmy damping (Q647195) (← links)
- Discussion on: ``State feedback fuzzy adaptive control for active shimmy damping'' (Q647197) (← links)
- Bifurcations of the self-exciting oscillations of a wheeled assembly about straight-line motion (Q2443376) (← links)
- Using nonlinear feedback control to improve aircraft nose landing gear shimmy performance (Q6100373) (← links)