Pages that link to "Item:Q2472404"
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The following pages link to Global optimal attitude estimation using uncertainty ellipsoids (Q2472404):
Displaying 17 items.
- State estimation for invariant systems on Lie groups with delayed output measurements (Q273967) (← links)
- Exponential convergence of a nonlinear attitude estimator (Q311879) (← links)
- Rigid body pose estimation based on the Lagrange-d'Alembert principle (Q313173) (← links)
- Robust adaptive terminal sliding mode control on \(\mathrm{SE(3)}\) for autonomous spacecraft rendezvous and docking (Q335745) (← links)
- Rigid body attitude estimation based on the Lagrange-d'Alembert principle (Q472575) (← links)
- A discrete-time observer design for spacecraft attitude determination using an orthogonality-preserving algorithm (Q540178) (← links)
- Optimal estimation for the satellite attitude using star tracker measurements (Q1076656) (← links)
- A GES attitude observer with single vector observations (Q1941266) (← links)
- Efficient geometric linearization of moving-base rigid robot dynamics (Q2086012) (← links)
- Attitude observer on the special orthogonal group with Earth velocity estimation (Q2327357) (← links)
- Ellipsoidal bounds on state trajectories for discrete-time systems with linear fractional uncertainties (Q2357944) (← links)
- Global attitude and gyro bias estimation based on set-valued observers (Q2439152) (← links)
- On the attitude estimation of nonholonomic wheeled mobile robots (Q2682310) (← links)
- Tightly coupled long baseline/ultra-short baseline integrated navigation system (Q2798516) (← links)
- Partial attitude and rate gyro bias estimation: observability analysis, filter design, and performance evaluation (Q2909410) (← links)
- Globally exponentially stable attitude observer with Earth velocity estimation (Q5215187) (← links)
- Set inversion and box contraction on Lie groups using interval analysis (Q6566771) (← links)
