Pages that link to "Item:Q2661921"
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The following pages link to The dynamics characteristics of flexible spacecraft and its closed-loop stability with passive control (Q2661921):
Displaying 9 items.
- Dynamics of a spacecraft with large flexible appendage constrained by multi-strut passive damper (Q315084) (← 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)
- Passive attitude control of flexible spacecraft from quaternion measurements (Q1411385) (← links)
- A characteristic modeling method of error-free compression for nonlinear systems (Q2138912) (← links)
- Longitudinal control for balloon-borne launched solar powered UAVs in near-space (Q2165427) (← 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)
- Robust and minimum norm dynamic compensator design for partial eigenvalues assignment problems in singular vibration systems (Q6053953) (← links)
- Mixed \(H_\infty\)/passive exponential synchronization for delayed memristive neural networks with switching event-triggered control (Q6130967) (← links)
