2014
DOI: 10.1186/bf03352458
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Calibration of the Ørsted vector magnetometer

Abstract: The vector fluxgate magnetometer of the Ørsted satellite is routinely calibrated by comparing its output with measurements of the absolute magnetic intensity from the Overhauser instrument, which is the second magnetometer of the satellite. We describe the method used for and the result obtained in that calibration. Using three years of data the agreement between the two magnetometers after calibration is 0.33 nT rms (corresponding to better than ±1 nT for 98% of the data, and better than ±2 nT for 99.94% of t… Show more

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Cited by 118 publications
(110 citation statements)
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“…This technique is exploited by satellites because the vector reference field is not available. Nevertheless, instruments are orbiting around the Earth (Olsen et al, 2003). The different scalar measurements from the scalar instrument can therefore be compared to the scalar values computed from the vector instrument.…”
Section: Dourbes D0 Baseline 2013mentioning
confidence: 99%
“…This technique is exploited by satellites because the vector reference field is not available. Nevertheless, instruments are orbiting around the Earth (Olsen et al, 2003). The different scalar measurements from the scalar instrument can therefore be compared to the scalar values computed from the vector instrument.…”
Section: Dourbes D0 Baseline 2013mentioning
confidence: 99%
“…VFM measurements are calibrated using those from the ASM similarly as already done in other satellite missions for magnetic field mapping purposes and which carried equivalent instrumentation (Olsen et al 2003;Yin and Lühr 2011). According to the traditional in-flight vector calibration of VFM fluxgate instruments, the raw data of the vector magnetometer are processed by applying an error model which takes into account of scale factors and their dependence on time and temperature, offsets and nonorthogonal angles between the sensor elements.…”
Section: Open Accessmentioning
confidence: 99%
“…Ørsted (Olsen et al 2003) was launched in February 1999 into an elliptical near-polar orbit with an inclination of 96.4°. Its current perigee and apogee are about 635 and 835 km, respectively, and its orbital period is about 99.5 min.…”
Section: Data Sourcesmentioning
confidence: 99%