Pages that link to "Item:Q2342528"
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The following pages link to Globally exponentially stable attitude and gyro bias estimation with application to GNSS/INS integration (Q2342528):
Displaying 16 items.
- State estimation for invariant systems on Lie groups with delayed output measurements (Q273967) (← links)
- Exponential convergence of a nonlinear attitude estimator (Q311879) (← links)
- Attitude estimation by multiplicative exogenous Kalman filter (Q1626910) (← links)
- Global exponential attitude and gyro bias estimation from vector measurements (Q1689158) (← links)
- Hybrid controller concept for dynamic positioning of marine vessels with experimental results (Q1797061) (← links)
- A GES attitude observer with single vector observations (Q1941266) (← links)
- Nonlinear state estimation for inertial navigation systems with intermittent measurements (Q2208564) (← links)
- Globally exponentially stable filters for source localization and navigation aided by direction measurements (Q2439113) (← links)
- Global attitude and gyro bias estimation based on set-valued observers (Q2439152) (← links)
- Attitude, body-fixed Earth rotation rate, and sensor bias estimation using single observations of direction of gravitational field (Q2663979) (← links)
- A nonlinear navigation observer using IMU and generic position information (Q2664245) (← 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)
- Data fusion‐based descriptor approach for attitude estimation under accelerated maneuvers (Q5215191) (← links)
- Design of inertial navigation systems for marine craft with adaptive wave filtering aided by triple‐redundant sensor packages (Q5348646) (← links)
- Finite‐time constrained attitude regulation for spacecraft formation with disturbances on SO(3)$$ SO(3) $$ (Q6190416) (← links)
