Pages that link to "Item:Q5240713"
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The following pages link to Observer-based continuous finite-time attitude control for rigid–flexible coupling satellites (Q5240713):
Displaying 6 items.
- Using of H-infinity control method in attitude control system of rigid-flexible satellite (Q613793) (← links)
- Speed control based on ESO for the pitching axis of satellite cameras (Q1792807) (← links)
- Agile attitude maneuver with active vibration-suppression for flexible spacecraft (Q2667427) (← links)
- Inertia‐free attitude stabilization for flexible spacecraft with active vibration suppression (Q3300450) (← links)
- (Q4649717) (← links)
- Research on active control of rigid-flexible coupling piezoelectric rectangular thin plate (Q6649688) (← links)