Pages that link to "Item:Q4864412"
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The following pages link to Feedback control logic for spacecraft eigenaxis rotations under slew rate and control constraints (Q4864412):
Displaying 10 items.
- Rigid-body attitude stabilization with attitude and angular rate constraints (Q1640734) (← links)
- Active eigen-orbit control (Q2725701) (← links)
- Time-optimal reorientation of the rigid spacecraft using a pseudospectral method integrated homotopic approach (Q2793927) (← links)
- Adaptive fuzzy PD+ control for attitude maneuver of rigid spacecraft (Q2821218) (← links)
- Analysis of the inertially symmetric rigid spacecraft time-optimal three-axis reorientation (Q2965295) (← links)
- Optimal non-linear feedback regulation of spacecraft angular momentum (Q3340584) (← links)
- Event-triggered integral sliding mode controller for rigid spacecraft attitude tracking with angular velocity constraint (Q5056567) (← links)
- Null‐space‐based optimal control reallocation for spacecraft stabilization under input saturation (Q5743794) (← links)
- Robust PID controller for flexible satellite attitude control under angular velocity and control torque constraint (Q6563461) (← links)
- Single saturated PD control for asymptotic attitude stabilisation of spacecraft (Q6611576) (← links)