Pages that link to "Item:Q2393561"
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The following pages link to Underactuated spacecraft angular velocity stabilization and three-axis attitude stabilization using two single gimbal control moment gyros (Q2393561):
Displaying 9 items.
- Controllability of an underactuated spacecraft with one thruster under disturbance (Q315234) (← links)
- Influence of flexible solar arrays on vibration isolation platform of control moment gyroscopes (Q315357) (← links)
- Attitude control for part actuator failure of agile small satellite (Q364167) (← links)
- On the attitude stabilization of a rigid spacecraft using two skew control moment gyros (Q494779) (← links)
- Attitude control of a rigid spacecraft with one variable-speed control moment gyro (Q740030) (← links)
- Controlling a satellite using single-gimbal control moment gyroscope during their spinning and braking (Q786153) (← links)
- Velocity-free spacecraft attitude stabilization using two control torques (Q2280946) (← links)
- Spacecraft attitude control using two control torques (Q2293286) (← links)
- Angular velocity stabilization of underactuated rigid satellites based on energy shaping (Q2667456) (← links)