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dc.contributor.authorDe Keyser, J.
dc.date2008
dc.date.accessioned2016-09-21T11:04:57Z
dc.date.available2016-09-21T11:04:57Z
dc.identifier.urihttps://orfeo.belnet.be/handle/internal/4325
dc.descriptionMulti-spacecraft missions allow the gradient of important physical quantities in the terrestrial environment to be determined. The gradient can be computed from four simultaneous measurements in a straightforward way, but this computation does not produce proper error estimates, making it hard to assess the meaningfulness of the result. Recently developed least-squares gradient computation techniques offer the possibility to obtain more precise results with all-inclusive error estimates, provided that information about the non-linearity of the space and time variations of the observed quantity is given. The present paper describes several heuristics for estimating these variations, thereby enabling a fully automatic computation of the gradient and the associated error estimates. The performance of these heuristics is illustrated with synthetic data corresponding to 4- and 10-spacecraft configurations.
dc.languageeng
dc.titleLeast-squares multi-spacecraft gradient calculation with automatic error estimation
dc.typeArticle
dc.subject.frascatiPhysical sciences
dc.audienceScientific
dc.subject.freeenvironmental gradient
dc.subject.freeerror analysis
dc.subject.freegradient analysis
dc.subject.freeheuristics
dc.subject.freeleast squares method
dc.subject.freespacecraft
dc.subject.freespatial variation
dc.subject.freetemporal variation
dc.subject.freeterrestrial environment
dc.source.titleAnnales Geophysicae
dc.source.volume26
dc.source.issue11
dc.source.page3295-3316
Orfeo.peerreviewedYes
dc.identifier.doi10.5194/angeo-26-3295-2008
dc.identifier.scopus2-s2.0-54849416433


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