Pages that link to "Item:Q5166492"
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The following pages link to High‐gain output feedback for a miniature UAV (Q5166492):
Displaying 7 items.
- Design of attitude control system for UAV based on feedback linearization and adaptive control (Q1718528) (← links)
- Robust \(D\)-stability controller design for a ducted fan unmanned aerial vehicle (Q1719063) (← links)
- Output feedback control design using extended high-gain observers and dynamic inversion with projection for a small scaled helicopter (Q2065230) (← links)
- Nonlinear feedback control of axisymmetric aerial vehicles (Q2409411) (← links)
- High‐gain observers in nonlinear feedback control (Q5166486) (← links)
- Stabilization of the planar vertical take‐off and landing using nonlinear feedback control (Q6092333) (← links)
- Bumpless‐transfer‐based fault tolerant control for the quadcopter: Piecewise homogeneous emission probability approach (Q6117441) (← links)