Attitude estimation by multiplicative exogenous Kalman filter

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

zbMATH Keywords

Kalman filterglobal exponential stabilitynonlinear observer and filter design

Mathematics Subject Classification ID

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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