1988
DOI: 10.1016/0273-1177(88)90141-x
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Analysis of multipoint magnetometer data

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Cited by 209 publications
(249 citation statements)
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“…In-flight calibrations on FGM data routinely determine the maximum error in the data to within 0.1 nT. The "Curlometer" technique has been developed to derive currents from four-point magnetic field measurements (Dunlop et al, 1988(Dunlop et al, , 2002Robert et al, 1998) based on MaxwellAmpere's law…”
Section: Introductionmentioning
confidence: 99%
See 1 more Smart Citation
“…In-flight calibrations on FGM data routinely determine the maximum error in the data to within 0.1 nT. The "Curlometer" technique has been developed to derive currents from four-point magnetic field measurements (Dunlop et al, 1988(Dunlop et al, , 2002Robert et al, 1998) based on MaxwellAmpere's law…”
Section: Introductionmentioning
confidence: 99%
“…Nevertheless, it was stable and mainly <0.5 (under red line) within the interval of the ring current. Dunlop et al (1988) suggested that the ratio Div(B)/|Curl(B)| can provide a quality estimate for J calculated in place of the unknown error (J calculated − J real ) when the shape and orientation of the spacecraft configuration is regular tetrahedron, and the magnetic field structure is nearly isotropic within the tetrahedron. The use of Div(B) does not give a direct indication of the actual error in the current estimate and is less relevant for distorted tetrahedral configurations.…”
Section: Introductionmentioning
confidence: 99%
“…The method to obtain two-dimensional pressure gradient is similar as calculating the magnetic gradient using the curlometer technique [Dunlop et al, 1988] but has been simplified to two dimensions.…”
Section: 1002/2014ja020186mentioning
confidence: 99%
“…But a fundamental problem always exists: how should the comparative information between spacecraft be built into any analysis? The determination of di erent properties demands di erent methods of coordination (Dunlop et al, 1988); often having a large overlap between them, with parameters in common. In terms of boundary analysis, although there is an apparent distinction between macroscopic parameters (such as motion, orientation and form) and the boundary structure itself (as sampled individually by each spacecraft), it is not always a priori obvious how spacecraft di erences are to be combined with time series information, except where the boundary is planar or`thin' (Dunlop and Woodward, 1998).…”
Section: Introductionmentioning
confidence: 99%