Pages that link to "Item:Q1040489"
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The following pages link to Design of discrete control system of flexible spacecraft maintaining robust stability of elastic oscillations (Q1040489):
Displaying 9 items.
- Using the method of invariant ellipsoids for linear robust output stabilization of spacecraft (Q647768) (← links)
- Two-level orientation control system of flexible spacecraft with active stabilization of structural elastic oscillations (Q1002975) (← links)
- Stabilization of a class of hybrid systems arising in flexible spacecraft (Q1061681) (← links)
- Output regulation of a flexible spacecraft with exponentially stable/unstable internal dynamics (Q1267267) (← links)
- Studying stability of the flexible spacecraft with a discrete control system (Q1778375) (← links)
- Using the method of phase biplane to study dynamics of interactions of the elastic structural oscillations of the flexible spacecraft with the control system (Q2371583) (← links)
- (Q3739012) (← links)
- Dissipative controllers for nonlinear multibody flexible space systems (Q4864375) (← links)
- Angular motion control of a large space structure with elastic elements (Q6185394) (← links)