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Real-Time Attitude-Independent Three-Axis Magnetometer Calibration
Author(s) -
John L. Crassidis,
Kok-Lam Lai,
Richard R. Harman
Publication year - 2005
Publication title -
journal of guidance control and dynamics
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 1.573
H-Index - 143
eISSN - 1533-3884
pISSN - 0731-5090
DOI - 10.2514/1.6278
Subject(s) - magnetometer , kalman filter , control theory (sociology) , calibration , spacecraft , computer science , extended kalman filter , algorithm , orbit determination , filter (signal processing) , mathematics , physics , global positioning system , computer vision , artificial intelligence , control (management) , quantum mechanics , magnetic field , telecommunications , statistics , astronomy
In this paper new real-time approaches for three-axis magnetometer sensor calibration are derived. These approaches rely on a conversion of the magnetometer-body and geomagnetic-reference vectors into an attitude independent observation by using scalar checking. The goal of the full calibration problem involves the determination of the magnetometer bias vector, scale factors and non-orthogonality corrections. Although the actual solution to this full calibration problem involves the minimization of a quartic loss function, the problem can be converted into a quadratic loss function by a centering approximation. This leads to a simple batch linear least squares solution. In this paper we develop alternative real-time algorithms based on both the extended Kalman filter and Unscented filter. With these real-time algorithms, a full magnetometer calibration can now be performed on-orbit during typical spacecraft mission-mode operations. Simulation results indicate that both algorithms provide accurate integer resolution in real time, but the Unscented filter is more robust to large initial condition errors than the extended Kalman filter. The algorithms are also tested using actual data from the Transition Region and Coronal Explorer (TRACE).

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