Pages that link to "Item:Q1881967"
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The following pages link to On the stability of a spacecraft with regard for its elastic oscillations (Q1881967):
Displaying 13 items.
- Investigation of the stabilization process for a multidimensional dynamical system with relay control (Q372288) (← links)
- Adaptive approach with the ``fast'' model for dynamics identification and forecasting problems for relay control of an elastic satellite (Q612073) (← links)
- Using the method of invariant ellipsoids for linear robust output stabilization of spacecraft (Q647768) (← links)
- Design of discrete control system of flexible spacecraft maintaining robust stability of elastic oscillations (Q1040489) (← links)
- Dynamic stability of a flexible spacecraft in the presence of nonlinear resonances (Q1326205) (← links)
- Oscillations in a relay control system with hysteresis and time dead zone (Q1602721) (← links)
- Analysis of a resonance liquid bridge oscillation on board of the international space station (Q1671498) (← links)
- Studying stability of the flexible spacecraft with a discrete control system (Q1778375) (← links)
- Design of the suboptimal profiled relay control of orientation of the spacecraft having elastic structural elements with regard for two oscillation tones (Q1778637) (← links)
- On stability of limit cycles in stabilization systems of spacecrafts with elastic rods (Q2017497) (← links)
- On the nonlinear stability of relative equilibria of the full spacecraft dynamics around an asteroid (Q2346789) (← 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)
- On the spacecraft attitude stabilization in the orbital frame (Q5403494) (← links)
