Assessing and ensuring GOES-R magnetometer accuracy
Author(s) -
Delano Carter,
Monica Todirita,
J. Kronenwetter,
Melissa Dahya,
Donald Chu
Publication year - 2016
Publication title -
proceedings of spie, the international society for optical engineering/proceedings of spie
Language(s) - English
Resource type - Conference proceedings
SCImago Journal Rank - 0.192
H-Index - 176
eISSN - 1996-756X
pISSN - 0277-786X
DOI - 10.1117/12.2228542
Subject(s) - magnetometer , offset (computer science) , calibration , spacecraft , physics , computer science , monte carlo method , sigma , control theory (sociology) , statistics , magnetic field , mathematics , artificial intelligence , control (management) , quantum mechanics , astronomy , programming language
The GOES-R magnetometer subsystem accuracy requirement is 1.7 nanoteslas (nT). During quiet times (100 nT), accuracy is defined as absolute mean plus 3 sigma error per axis. During storms (300 nT), accuracy is defined as absolute mean plus 2 sigma error per axis. Error comes both from outside the magnetometers, e.g. spacecraft fields and misalignments, as well as inside, e.g. zero offset and scale factor errors. Because zero offset and scale factor drift over time, it will be necessary to perform annual calibration maneuvers. To predict performance before launch, we have used Monte Carlo simulations and covariance analysis. With the proposed calibration regimen, both suggest that the magnetometer subsystem will meet its accuracy requirements.
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