Pages that link to "Item:Q494779"
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The following pages link to On the attitude stabilization of a rigid spacecraft using two skew control moment gyros (Q494779):
Displaying 14 items.
- Chaotic attitude analysis of a satellite via Lyapunov exponents and its robust nonlinear control subject to disturbances and uncertainties (Q331234) (← links)
- Dual-quaternion-based adaptive motion tracking of spacecraft with reduced control effort (Q331254) (← links)
- Model predictive control of rigid spacecraft with two variable speed control moment gyroscopes (Q680974) (← 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)
- Adaptive integral sliding mode control for spacecraft attitude tracking with actuator uncertainty (Q1660822) (← links)
- Kinematics and dynamics of a double-gimbaled control moment gyroscope (Q1854188) (← links)
- Velocity-free spacecraft attitude stabilization using two control torques (Q2280946) (← links)
- Underactuated spacecraft angular velocity stabilization and three-axis attitude stabilization using two single gimbal control moment gyros (Q2393561) (← links)
- Small-time local controllability of spacecraft attitude using control moment gyros (Q2409421) (← links)
- Agile attitude maneuver with active vibration-suppression for flexible spacecraft (Q2667427) (← links)
- Spacecraft attitude control by combination of various torquers (Q3644975) (← links)
- Approach to control moment gyroscope steering using feedback linearization (Q3984655) (← links)
- Robust control for uncertain impulsive systems with input constraints and external disturbance (Q6092323) (← links)
