Pages that link to "Item:Q1634453"
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The following pages link to Robust output feedback attitude tracking control for rigid-flexible coupling spacecraft (Q1634453):
Displaying 11 items.
- Robust \(H_\infty \) output feedback control for attitude stabilization of a flexible spacecraft (Q332763) (← links)
- Adaptive robust tracking for flexible spacecraft in presence of disturbances (Q1273906) (← links)
- Nonlinear stochastic position and attitude filter on the special Euclidean group 3 (Q2416688) (← links)
- Robust and adaptive variable structure output feedback control of uncertain systems with input nonlinearity (Q2440633) (← links)
- Agile attitude maneuver with active vibration-suppression for flexible spacecraft (Q2667427) (← links)
- An optimal dynamic output feedback controller for a flexible spacecraft (Q3469023) (← links)
- Robust attitude tracking control of flexible spacecraft for achieving globally asymptotic stability (Q3497676) (← links)
- (Q4574933) (← links)
- Observer-based continuous finite-time attitude control for rigid–flexible coupling satellites (Q5240713) (← links)
- Decoupled Tracking Control for a Flexible Multi-body Satellite with Solar Panels and Manipulator (Q5377300) (← links)
- Research on active control of rigid-flexible coupling piezoelectric rectangular thin plate (Q6649688) (← links)
