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Assessing and Ensuring GOES-R Magnetometer AccuracyThe 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. During storms (300 nT), accuracy is defined as absolute mean plus 2 sigma. 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. Both behave as expected, and their accuracy predictions agree within 30%. With the proposed calibration regimen, both suggest that the GOES-R magnetometer subsystem will meet its accuracy requirements.
Document ID
20160004691
Acquisition Source
Goddard Space Flight Center
Document Type
Conference Paper
Authors
Carter, Delano R.
(Thearality inc. Glendale, AZ, United States)
Todirita, Monica
(National Oceanic and Atmospheric Administration Silver Spring, MD, United States)
Kronenwetter, Jeffrey
(Chesapeake Aerospace, LLC Grasonville, MD, United States)
Chu, Donald
(Chesapeake Aerospace, LLC Grasonville, MD, United States)
Date Acquired
April 6, 2016
Publication Date
April 4, 2016
Subject Category
Instrumentation And Photography
Report/Patent Number
GSFC-E-DAA-TN30636
Report Number: GSFC-E-DAA-TN30636
Meeting Information
Meeting: SPIE Asia-Pacific Remote Sensing
Location: New Delhi
Country: India
Start Date: April 4, 2016
End Date: April 7, 2016
Sponsors: International Society for Optical Engineering
Funding Number(s)
CONTRACT_GRANT: NNG15CR65C
CONTRACT_GRANT: NNG12CR29C
CONTRACT_GRANT: NNG14CR58C
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Magnetometer
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