Attitude estimation by multiplicative exogenous Kalman filter
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Publication:1626910
DOI10.1016/j.automatica.2018.05.038zbMath1402.93250OpenAlexW2808933661MaRDI QIDQ1626910
Tor Arne Johansen, Ingrid Schjølberg, Bård Nagy Stovner, Thor I. Fossen
Publication date: 21 November 2018
Published in: Automatica (Search for Journal in Brave)
Full work available at URL: http://hdl.handle.net/11250/2581721
Filtering in stochastic control theory (93E11) Nonlinear systems in control theory (93C10) Estimation and detection in stochastic control theory (93E10) Lyapunov and other classical stabilities (Lagrange, Poisson, (L^p, l^p), etc.) in control theory (93D05) Observability (93B07)
Related Items (4)
Attitude estimation based on robust information cubature quaternion filter ⋮ A geometric framework for rigid body attitude estimation ⋮ Two-stage exogenous Kalman filter for time-varying fault estimation of satellite attitude control system ⋮ Cauchy kernel-based maximum correntropy Kalman filter
Cites Work
- Generalization of the Sherman-Morrison-Woodbury formula involving the Schur complement
- A GES attitude observer with single vector observations
- Fundamentals of spacecraft attitude determination and control
- Globally exponentially stable attitude and gyro bias estimation with application to GNSS/INS integration
- Matrix Tricks for Linear Statistical Models
- Optimized TRIAD Algorithm for Attitude Determination
- A globally convergent angular velocity observer for rigid body motion
- Nonlinear Complementary Filters on the Special Orthogonal Group
- A coupled nonlinear spacecraft attitude controller and observer with an unknown constant gyro bias and gyro noise
- Attitude Estimation Using Biased Gyro and Vector Measurements With Time-Varying Reference Vectors
- Generalized Inverses and Ranks of Block Matrices
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