Pages that link to "Item:Q4207839"
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The following pages link to Design of a helicopter output feedback control law using modal and structured-robustness techniques (Q4207839):
Displaying 3 items.
- Output sliding mode-based stabilization of underactuated 3-DOF helicopter prototype and its experimental verification (Q1660413) (← links)
- Performance bounds of discrete-time LQ systems with structured uncertainties (Q4294377) (← links)
- Robust output tracking control of a laboratory helicopter for automatic landing (Q5499828) (← links)