Real-Time Attitude-Independent Three-Axis Magnetometer Calibration

Калибровка трёхосевого магнитометра в реальном времени, независимая от ориентации
John L. Crassidis, Kok-Lam Lai, Richard R. Harman
2005-01-01

Unscented Kalman filterattitude-independent observationextended Kalman filterspacecraft on-orbit calibrationthree-axis magnetometer calibration
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).
1
A centering approximation transforms the full quartic-loss calibration problem into a quadratic-loss problem solvable by batch linear least squares.
2
Extended Kalman filter and Unscented filter algorithms enable full three-axis magnetometer calibration in real time during spacecraft mission-mode operations.
3
Simulations show both real-time algorithms achieve accurate integer-resolution calibration, while the Unscented filter is more robust to large initial-condition errors.
4
The algorithms were additionally validated using actual data from the Transition Region and Coronal Explorer (TRACE).
5
The proposed calibration methods convert magnetometer-body and geomagnetic-reference vectors into attitude-independent observations using scalar checking.

three-axis magnetometer sensors operating on spacecraft

real-time full calibration, including bias, scale-factor, and non-orthogonality estimation, and the robustness of extended Kalman and Unscented filter algorithms to initialization errors

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2005-01-01
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Authors
John L. Crassidis
Kok-Lam Lai
Richard R. Harman
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