Pages that link to "Item:Q2193377"
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The following pages link to Finite time output feedback attitude tracking control for rigid body based on extended state observer (Q2193377):
Displaying 10 items.
- Finite-time output feedback attitude control for rigid spacecraft under control input saturation (Q344632) (← links)
- A discrete-time observer design for spacecraft attitude determination using an orthogonality-preserving algorithm (Q540178) (← links)
- Output feedback control for attitude tracking (Q1606511) (← links)
- Speed control based on ESO for the pitching axis of satellite cameras (Q1792807) (← links)
- Disturbance observer-based saturated fixed-time pose tracking for feature points of two rigid bodies (Q2165971) (← links)
- Spacecraft output feedback attitude control based on extended state observer and adaptive dynamic programming (Q2423888) (← links)
- Spacecraft time-delay state feedback control based on extended state observer (Q2825204) (← links)
- Attitude observer-based robust control for a twin rotor system (Q2868788) (← links)
- Finite-time angular velocity observers for rigid-body attitude tracking with bounded inputs (Q2956841) (← links)
- Attitude control via a feedback integrator based observer (Q6163993) (← links)
