Attitude estimation by multiplicative exogenous Kalman filter
type: Item
instance of: scholarly article
title: Attitude estimation by multiplicative exogenous Kalman filter
zbMATH Open document ID: 1402.93250
author: Bård Nagy Stovner
author: T. A. Johansen
author: Thor I. Fossen
author: Ingrid Schjølberg
published in: Automatica
publication date: 2018-11-21T00:00:00Z
full work available at URL: http://hdl.handle.net/11250/2581721
Mathematics Subject Classification ID: 93E11
Mathematics Subject Classification ID: 93E10
Mathematics Subject Classification ID: 93B07
Mathematics Subject Classification ID: 93C10
Mathematics Subject Classification ID: 93D05
zbMATH DE Number: 6982644
zbMATH Keywords: nonlinear observer and filter design
zbMATH Keywords: global exponential stability
zbMATH Keywords: Kalman filter
MaRDI profile type: Publication
OpenAlex ID: W2808933661
cites work: Optimized TRIAD Algorithm for Attitude Determination
cites work: A GES attitude observer with single vector observations
cites work: Attitude Estimation Using Biased Gyro and Vector Measurements With Time-Varying Reference Vectors
cites work: Globally exponentially stable attitude and gyro bias estimation with application to GNSS/INS integration
cites work: Nonlinear Complementary Filters on the Special Orthogonal Group
cites work: Fundamentals of spacecraft attitude determination and control
cites work: Generalized Inverses and Ranks of Block Matrices
cites work: Matrix Tricks for Linear Statistical Models
cites work: A globally convergent angular velocity observer for rigid body motion
cites work: A coupled nonlinear spacecraft attitude controller and observer with an unknown constant gyro bias and gyro noise
cites work: Generalization of the Sherman-Morrison-Woodbury formula involving the Schur complement
DOI: 10.1016/J.AUTOMATICA.2018.05.038
description: scientific article; zbMATH DE number 6982644