Pages that link to "Item:Q2293286"
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The following pages link to Spacecraft attitude control using two control torques (Q2293286):
Displaying 13 items.
- Near-minimum-time control of asymmetric rigid spacecraft using two controls (Q466284) (← links)
- On the attitude stabilization of a rigid spacecraft using two skew control moment gyros (Q494779) (← links)
- Control of underactuated spacecraft with bounded inputs (Q1576500) (← links)
- A novel approach to the attitude control of axisymmetric spacecraft (Q1899594) (← links)
- A quick position control strategy based on optimization algorithm for a class of first-order nonholonomic system (Q2198207) (← 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)
- Spacecraft output feedback attitude control based on extended state observer and adaptive dynamic programming (Q2423888) (← links)
- Robust nonlinear attitude tracking control of an underactuated spacecraft under saturation and time-varying uncertainties (Q2667491) (← links)
- Attitude Motion of Asymmetric Dual-Spin Spacecraft (Q3327802) (← links)
- Attitude Control of a Spacecraft with Two Reaction Wheels (Q5699632) (← links)
- Position control with zero residual vibration for two degrees-of-freedom flexible systems based on motion trajectory optimization (Q6066014) (← links)
- Adaptive quantized sliding mode attitude tracking control for flexible spacecraft with input dead-zone via Takagi-Sugeno fuzzy approach (Q6154807) (← links)
