TY - GEN
T1 - Three-axis magnetometer calibration using total least squares
AU - Crassidis, John L.
AU - Cheng, Yang
N1 - Publisher Copyright:
© 2020, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2020
Y1 - 2020
N2 - In this paper attitude-independent three-axis magnetometer (TAM) sensor calibration algorithms are presented from a total least squares approach. One algorithm estimates biases only, while the other performs full calibration, which includes biases, scale factors and nonorthog-onality corrections. It is shown that the TAM calibration problem using a standard least squares point-of-view is statistically inconsistent because the effective measurement variance is a function of the calibration parameters. This inconsistency is overcome by using the total least squares formulation. The error-covariance of the calibration parameters is also derived, which is shown to be equivalent to the standard least squares formation to within first-order terms. Also, the covariance of the measurement-to-estimate residual vector is derived, which cannot be accomplished using a standard least squares approach. This covariance is useful to quantify the effects of the measurement covariance for attitude determination in real-world situations. Both simulated and experimental results are shown to assess the performance of the TAM calibration algorithms, as well as the derived covariance expressions.
AB - In this paper attitude-independent three-axis magnetometer (TAM) sensor calibration algorithms are presented from a total least squares approach. One algorithm estimates biases only, while the other performs full calibration, which includes biases, scale factors and nonorthog-onality corrections. It is shown that the TAM calibration problem using a standard least squares point-of-view is statistically inconsistent because the effective measurement variance is a function of the calibration parameters. This inconsistency is overcome by using the total least squares formulation. The error-covariance of the calibration parameters is also derived, which is shown to be equivalent to the standard least squares formation to within first-order terms. Also, the covariance of the measurement-to-estimate residual vector is derived, which cannot be accomplished using a standard least squares approach. This covariance is useful to quantify the effects of the measurement covariance for attitude determination in real-world situations. Both simulated and experimental results are shown to assess the performance of the TAM calibration algorithms, as well as the derived covariance expressions.
UR - https://www.scopus.com/pages/publications/85092398116
U2 - 10.2514/6.2020-1688
DO - 10.2514/6.2020-1688
M3 - Conference contribution
AN - SCOPUS:85092398116
SN - 9781624105951
T3 - AIAA Scitech 2020 Forum
SP - 1
EP - 24
BT - AIAA Scitech 2020 Forum
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Scitech Forum, 2020
Y2 - 6 January 2020 through 10 January 2020
ER -