Pages that link to "Item:Q2667427"
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The following pages link to Agile attitude maneuver with active vibration-suppression for flexible spacecraft (Q2667427):
Displaying 13 items.
- Influence of flexible solar arrays on vibration isolation platform of control moment gyroscopes (Q315357) (← links)
- Sliding mode maneuvering control and active vibration damping of three-axis stabilized flexible spacecraft with actuator dynamics (Q840431) (← links)
- Simultaneous maneuver and vibration suppression of flexible spacecraft (Q1113861) (← links)
- Passive attitude control of flexible spacecraft from quaternion measurements (Q1411385) (← links)
- The coupling characteristic investigation of double-gimbal magnetically suspended control moment gyro used on agile maneuver spacecraft (Q1665210) (← links)
- Fixed-time sliding mode attitude control of a flexible spacecraft with rotating appendages connected by magnetic bearing (Q2130302) (← links)
- Finite-time attitude maneuvering and vibration suppression of flexible spacecraft (Q2205531) (← links)
- Integrated vibration suppression attitude control for flexible spacecrafts with internal liquid sloshing (Q2229303) (← links)
- Observer based active vibration control of flexible space structures with prescribed performance (Q2297389) (← links)
- Inertia‐free attitude stabilization for flexible spacecraft with active vibration suppression (Q3300450) (← links)
- Robust microvibration mitigation and pointing performance analysis for high stability spacecraft (Q4644850) (← links)
- Hybrid control of attitude maneuver and structural vibration for a large phased array antenna satellite (Q6190549) (← links)
- Multi-objective design of parametric equivalent-input-disturbance approaches with application to vehicle suspension systems (Q6559374) (← links)
