NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Crucial Role of Thermal Gradients in MMS Fluxgate In-Flight CalibrationTo meet the science goals of the Magnetospheric Multiscale (MMS) mission, the Fluxgate Magnetometer (FGM) must measure the ambient magnetic field with an accuracy of 0.1 nT. On a typical MMS orbit, the offsets (or zero levels) of the 3-axis FGM can vary by ~0.5 nT (exclusive of periods in Earth shadow). Previous studies have shown that these variations can be characterized as functions of sensor temperature, TS, and can thus be corrected to within 0.2 nT in the spin plane using in-flight calibration techniques (Bromund, et al., 2016, https://ntrs.nasa.gov/citations/20160014711). In that presentation, we noted two significant observations:
A distinct function of TS must be used to characterize offsets during shadow: offsets at a given TScan differ by as much as 2 nT in shadow vs sunlight.
Offsets change after maneuvers, without a commensurate change in TS . These changes can be as large as 2 nT.
We now note a third, related observation:

Offsets increase with proximity to the earth even when TS is constant, resulting in variations of ~0.2 nT at 4-5 Earth radii (RE)
These effects are evidence that offsets are a multivariate function of TS and another factor, namely: thermal gradients. Due to the spacecraft spin, the Earth and the Sun each provide a relatively constant thermal input onto one instrument face while the opposite face remains in shadow, thus giving rise to thermal gradients. The thermal gradient depend on the orientation of the spin axis relative to the Earth or Sun. We observe that offsets vary by as much as 0.17 nT/degree as a function of the tilt of the spin axis towards the Sun. Thermal input from the Earth is dominated by Outgoing Longwave Radiation (OLR). Due to the proximity to Earth, the inverse proportion of the distance squared is a significant factor in the thermal gradient attributed to Earth OLR. We find that offsets can be corrected to <0.05 nT accuracy near perigee when accounting for these factors using empirically determined constants of proportionality that account for differences in emissivity of the top and bottom faces of the sensor to OLR (as well as other thermal effects).

The changes in offset associated with thermal gradient are of the same order of magnitude as effects that were formerly attributed to sensor temperature alone, and thus both parameters are necessary to characterize the FGM offsets.
Document ID
20210025148
Acquisition Source
Goddard Space Flight Center
Document Type
Poster
Authors
Kenneth R Bromund
(Goddard Space Flight Center Greenbelt, Maryland, United States)
Bobby G Huang
(Adnet Systems (United States) Bethesda, Maryland, United States)
Brian J Anderson
(Johns Hopkins University Baltimore, Maryland, United States)
Guan Le
(Goddard Space Flight Center Greenbelt, Maryland, United States)
Mark Hubbert
(University of California, Los Angeles Los Angeles, California, United States)
Hanying Wei
(University of California, Los Angeles Los Angeles, California, United States)
Robert J Strangeway
(University of California, Los Angeles Los Angeles, California, United States)
Christopher T Russell
(University of California, Los Angeles Los Angeles, California, United States)
Rommel Zara
(Vertex Aerospace LLC)
Santino Rosanova
(Vertex Aerospace LLC)
Ferdinand Plaschke
(IWF ÖAW)
David Fischer
(Space Research Institute Graz, Austria)
Werner Magnes
(Space Research Institute Graz, Austria)
Date Acquired
November 30, 2021
Subject Category
Spacecraft Instrumentation And Astrionics
Report/Patent Number
SH35D-2103
Meeting Information
Meeting: AGU Fall Meeting 2021
Location: New Orleans, LA
Country: US
Start Date: December 13, 2021
End Date: December 17, 2021
Sponsors: American Geophysical Union
Funding Number(s)
WBS: 943396.04.08.03.04
Distribution Limits
Public
Copyright
Use by or on behalf of the US Gov. Permitted.
Technical Review
Single Expert
No Preview Available