Pages that link to "Item:Q5156970"
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The following pages link to Vibration Control for Flexible Spacecraft using Multi Impulse Robust Input Shaper and Optimal Control Method (Q5156970):
Displaying 5 items.
- Robust input shaping control for multi-mode flexible structures using neuro-sliding mode output feedback control (Q378642) (← links)
- Reduction of residual vibrations in a rotating flexible beam (Q1773269) (← links)
- (Q4623546) (← links)
- Continuous robust fault‐tolerant control and vibration suppression for flexible spacecraft without angular velocity (Q5241719) (← links)
- Manoeuvring and vibration reduction of a flexible spacecraft integrating optimal sliding mode controller and distributed piezoelectric sensors/actuators (Q5300367) (← links)