Pages that link to "Item:Q1606511"
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The following pages link to Output feedback control for attitude tracking (Q1606511):
Displaying 19 items.
- Finite-time output feedback attitude control for rigid spacecraft under control input saturation (Q344632) (← links)
- Hybrid attitude tracking of rigid bodies without angular velocity measurement (Q450671) (← links)
- A discrete-time observer design for spacecraft attitude determination using an orthogonality-preserving algorithm (Q540178) (← links)
- Spacecraft attitude control using magnetic actuators (Q705161) (← links)
- Output attitude tracking for flexible spacecraft (Q1858888) (← links)
- On the stability and stabilization of quaternion equilibria of rigid bodies (Q1932707) (← links)
- Robust and fault-tolerant spacecraft attitude control based on an extended-observer design (Q2089114) (← links)
- Spacecraft relative rotation tracking without angular velocity measurements (Q2390570) (← links)
- Rigid body attitude control with inclinometer and low-cost gyro measurements (Q2503500) (← links)
- Finite-time optimal tracking control for dynamic systems on Lie groups (Q2790010) (← links)
- Finite-time formation tracking control for multiple vehicles: a motion planning approach (Q2820458) (← links)
- Passivity Based Attitude Control of Rigid Bodies (Q2930770) (← links)
- The attitude control problem (Q3986170) (← links)
- (Q4921302) (← links)
- Output feedback control for rigid-body attitude with constant disturbances (Q5265937) (← links)
- A tracking system with space virtual feedback (Q5322621) (← links)
- Adaptive tracking control using synthesized velocity from attitude measurements (Q5935489) (← links)
- Rigid body attitude tracking without angular velocity feedback (Q5940887) (← links)
- Attitude control via a feedback integrator based observer (Q6163993) (← links)
