2012
DOI: 10.1071/eg12005
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Resolution analyses for selecting an appropriate airborne electromagnetic (AEM) system

Abstract: The choice of an appropriate airborne electromagnetic system for a given task should be based on a comparative analysis of candidate systems, consisting of both theoretical considerations and field studies including test lines.It has become common practice to quantify the system resolution for a series of models relevant to the survey area by comparing the sum over the data of squares of noise-normalised derivatives. We compare this analysis method with a resolution analysis based on the posterior covariance m… Show more

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Cited by 15 publications
(15 citation statements)
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“…The surface nuclear magnetic resonance (SNMR) inverse problem is non-linear (equation ( 2)), and although the methodology of using the covariance matrix is strictly valid only for linear inverse problems, it has been successfully applied for non-linear inverse problems (Behroozmand et al 2013;Christensen and Dodds 2007;Christensen and Lawrie 2012). We decided to investigate the model space using a genetic algorithm (GA) in order to ensure that the linearized covariance calculation gives acceptable results.…”
Section: Resultsmentioning
confidence: 99%
See 1 more Smart Citation
“…The surface nuclear magnetic resonance (SNMR) inverse problem is non-linear (equation ( 2)), and although the methodology of using the covariance matrix is strictly valid only for linear inverse problems, it has been successfully applied for non-linear inverse problems (Behroozmand et al 2013;Christensen and Dodds 2007;Christensen and Lawrie 2012). We decided to investigate the model space using a genetic algorithm (GA) in order to ensure that the linearized covariance calculation gives acceptable results.…”
Section: Resultsmentioning
confidence: 99%
“…The parameter uncertainty estimates are then obtained by the square root of the diagonal elements of C est . A similar approach for accessing the parameter uncertainty has been reported in (Christensen and Dodds 2007;Christensen and Lawrie 2012).…”
Section: Model Parameter Uncertaintymentioning
confidence: 95%
“…A traditional approach used to define the noise of an electronic system requires noise measures for each component of the system and an understanding of how each component contributes to overall system noise. Due to the complexity of AEM systems this approach is difficult to undertake and therefore noise is typically approximated by analysing observed data from multiple flights (Brodie & Fisher, 2008;Christensen & Lawrie, 2012;Green & Lane, 2003). Using this method the additive noise term is identified as the clearest indicator of system noise and resolvability.…”
Section: Noisementioning
confidence: 99%
“…The method by Green & Lane (2003), requires the estimation of a system noise level by analysis of the standard deviation of data measured at high altitude (additive noise) and the repeatability of data measured on multiple occasions over the same ground (multiplicative noise). Given the relative simplicity and robustness of this method, it is a regularly used approach for estimating the noise present in AEM data sets (see, for example, Annetts & Hauser, 2015;Brodie & Fisher, 2008;Brodie & Sambridge, 2009;Christensen & Lawrie, 2013;Ley-Cooper et al, 2015). The method developed by Auken et al (2009), requires the allocation of noise levels or removal of noisy data points in a dataset which is typically done via a manual process.…”
Section: Introductionmentioning
confidence: 99%