Pages that link to "Item:Q6100373"
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The following pages link to Using nonlinear feedback control to improve aircraft nose landing gear shimmy performance (Q6100373):
Displaying 8 items.
- Canonical description of the control system in the shimmy problem for the landing gear wheels of an aircraft (Q366905) (← links)
- State feedback fuzzy adaptive control for active shimmy damping (Q647195) (← links)
- Discussion on: ``State feedback fuzzy adaptive control for active shimmy damping'' (Q647197) (← links)
- Interaction of torsion and lateral bending in aircraft nose landing gear shimmy (Q1041883) (← links)
- Modeling and adaptive control of magneto-rheological buffer system for aircraft landing gear (Q2009959) (← links)
- Nonlinear energy sink to enhance the landing gear shimmy performance (Q2234550) (← links)
- Influence of variable side-stay geometry on the shimmy dynamics of an aircraft dual-wheel main landing gear (Q2871361) (← links)
- Enhanced vehicle shimmy performance using inerter-based suppression mechanism (Q6143093) (← links)