Pages that link to "Item:Q1326205"
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The following pages link to Dynamic stability of a flexible spacecraft in the presence of nonlinear resonances (Q1326205):
Displaying 10 items.
- Parametric excitation induced by solar pressure torque on the roll-yaw attitude motion of a gravity-gradient stabilized spacecraft (Q642415) (← links)
- Stabilization of a class of hybrid systems arising in flexible spacecraft (Q1061681) (← links)
- Analysis of a resonance liquid bridge oscillation on board of the international space station (Q1671498) (← links)
- On the stability of a spacecraft with regard for its elastic oscillations (Q1881967) (← links)
- Stability of nonlinear vibrations of a deploying flexible beam from a spacecraft (Q1969076) (← links)
- Nonlinear dynamic modeling and responses of a cable dragged flexible spacecraft (Q2137108) (← links)
- Analytical and experimental investigations of a space antenna system of four DOFs with internal resonances (Q2207961) (← 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)
- Estimation of the Probability of Capture into Resonance and Parametric Analysis in the Descent of an Asymmetric Spacecraft in an Atmosphere (Q4558318) (← links)
- Instability tests, Lyapunov's direct method, and exact stability boundaries for flexible satellites (Q4841473) (← links)
