Pages that link to "Item:Q617154"
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The following pages link to Application of output feedback sliding mode control to active flutter suppression of two-dimensional airfoil (Q617154):
Displaying 8 items.
- High-order sliding mode controller with backstepping design for aeroelastic systems (Q430490) (← links)
- Flutter instability and active aeroelastic control with time delay for a two-dimensional airfoil (Q2063426) (← links)
- Sliding mode control of directly excited structural dynamic model of twin-tailed fighter aircraft (Q2068220) (← links)
- The sliding mode control for an airfoil system driven by harmonic and colored Gaussian noise excitations (Q2307005) (← links)
- Active control of hypersonic airfoil flutter via adaptive fuzzy sliding mode method (Q2832371) (← links)
- Fault-Tolerant Control for Flutter of Airfoil Subject to Input Saturation (Q2960143) (← links)
- Analytical and Experimental Aeroelastic Wing Flutter Analysis and Suppression (Q2972416) (← links)
- (Q3561504) (← links)