Articles | Volume 10, issue 1
https://doi.org/10.5194/gi-10-13-2021
https://doi.org/10.5194/gi-10-13-2021
Research article
 | 
27 Jan 2021
Research article |  | 27 Jan 2021

Error estimate for fluxgate magnetometer in-flight calibration on a spinning spacecraft

Yasuhito Narita, Ferdinand Plaschke, Werner Magnes, David Fischer, and Daniel Schmid

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AR: Author's response | RR: Referee report | ED: Editor decision
AR by Yasuhito Narita on behalf of the Authors (10 Dec 2020)  Author's response   Manuscript 
ED: Publish as is (12 Dec 2020) by Valery Korepanov
AR by Yasuhito Narita on behalf of the Authors (12 Dec 2020)
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Short summary
The systematic error of calibrated fluxgate magnetometer data is studied for a spinning spacecraft. The major error comes from the offset uncertainty when the ambient magnetic field is low, while the error represents the combination of non-orthogonality, misalignment to spacecraft reference direction, and gain when the ambient field is high. The results are useful in developing future high-precision magnetometers and an error estimate in scientific studies using magnetometer data.