Pages that link to "Item:Q813865"
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The following pages link to Output feedback modular adaptive control of a nonlinear prototypical wing section (Q813865):
Displaying 5 items.
- Adaptive boundary control of store induced oscillations in a flexible aircraft wing (Q290876) (← links)
- Adaptive feedback linearization for the control of a typical wing section with structural nonlinearity (Q1307800) (← links)
- Adaptive control of a nonlinear prototypical wing section with reduced order observer (Q1961286) (← links)
- Parameter estimation of unstable, limit cycling systems using adaptive feedback linearization: example of delta wing roll dynamics (Q2899178) (← links)
- Ill-matched timescales in coupled systems can induce oscillation suppression (Q6557702) (← links)