Pages that link to "Item:Q2017654"
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The following pages link to Dynamics of spacecraft with elastic and dissipative elements in the attitude control mode (Q2017654):
Displaying 13 items.
- A mathematical model for the angular motion of large space structures with gyroscopic drive for an active compensation of elastic oscillations (Q656265) (← links)
- Dynamic features of flexible spacecraft control in process of its transformation into a large space structure (Q1002952) (← links)
- Methods of estimating the envelope of elastic oscillations of the flexible spacecraft (Q1778643) (← links)
- Controlling the one-dimensional motion of hybrid vibrational rod systems (Q1792403) (← links)
- On the stability of a spacecraft with regard for its elastic oscillations (Q1881967) (← links)
- Dynamical modeling and attitude analysis for the spacecraft with lateral solar arrays (Q2307026) (← 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)
- Dissipative Rigids in Gyrodynamics (Q3687782) (← links)
- Uniform damping control of spacecraft (Q3745730) (← links)
- ATTITUDE DRIFT OF TORQUE-FREE FLEXIBLE GYROS USING THE VISCOUS DAMPING MODEL (Q3823166) (← links)
- Rigid-body dynamics from the Euler equations to the attitude control of spacecraft in the works of scientists from Saint Petersburg State University. I (Q6060227) (← links)
- Attitude evolution of a dual-liquid-filled spacecraft with internal energy dissipation (Q6166386) (← links)
- Angular motion control of a large space structure with elastic elements (Q6185394) (← links)
