Pages that link to "Item:Q315357"
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The following pages link to Influence of flexible solar arrays on vibration isolation platform of control moment gyroscopes (Q315357):
Displaying 7 items.
- Combined control of fast attitude maneuver and stabilization for large complex spacecraft (Q318000) (← links)
- Vibration isolation performance evaluation of the discrete whole-spacecraft vibration isolation platform for flexible spacecrafts (Q399269) (← links)
- Attitude control of a rigid spacecraft with one variable-speed control moment gyro (Q740030) (← links)
- The transmissibility of nonlinear energy sink based on nonlinear output frequency-response functions (Q2005043) (← links)
- A hybrid multi-degree-of-freedom vibration isolation platform for spacecrafts by the linear active disturbance rejection control (Q2659552) (← links)
- Micro-vibration modeling and analysis of single-gimbal control moment gyros (Q2684128) (← links)
- Active vibration isolation based on model reference adaptive control (Q5172543) (← links)