Pages that link to "Item:Q1002975"

The following pages link to Two-level orientation control system of flexible spacecraft with active stabilization of structural elastic oscillations (Q1002975):

Displaying 8 items.

• Estimating nonmeasurable coordinates of elastic oscillations for large space constructions with a gyroforce engine (Q386933) (← links)
• Design of discrete control system of flexible spacecraft maintaining robust stability of elastic oscillations (Q1040489) (← links)
• Methods for the vibration determination and parameter identification of spacecraft with flexible structures (Q1745820) (← links)
• Synthesis of an active compensation algorithm for elastic oscillations with nonstationary parameters for deformable spacecrafts (Q2261758) (← links)
• Algorithms of stabilization of a spacecraft with flexible elements (Q2290518) (← 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)
• Control of the angular motion of a semiactive bundle of bodies relying on the estimates of nonmeasurable coordinated obtained by Kalman filtering methods (Q2487581) (← links)
• Nonlinear control with distributed delay for the angular stabilization of a rigid body (Q2688541) (← links)