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A dual estimate method for aeromagnetic compensation

机译:一种用于航空磁性补偿的双重估计方法

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摘要

Scalar aeromagnetic surveys have played a vital role in prospecting. However, before analysis of the surveys' aeromagnetic data is possible, the aircraft's magnetic interference should be removed. The extensively adopted linear model for aeromagnetic compensation is computationally efficient but faces an underfitting problem. On the other hand, the neural model proposed by Williams is more powerful at fitting but always suffers from an overfitting problem. This paper starts off with an analysis of these two models and then proposes a dual estimate method to combine them together to improve accuracy. This method is based on an unscented Kalman filter, but a gradient descent method is implemented over the iteration so that the parameters of the linear model are adjustable during flight. The noise caused by the neural model's overfitting problem is suppressed by introducing an observation noise.
机译:标量在勘探中发挥了至关重要的作用。 然而,在分析调查的航空磁数据之前,应拆除飞机的磁干扰。 广泛采用的航空磁性补偿线性模型是计算效率,但面临磨损问题。 另一方面,威廉姆斯提出的神经模型在适应时更强大,但总是遭受过度装备的问题。 本文开始分析这两种模型,然后提出了一种将它们组合在一起以提高准确性的双重估计方法。 该方法基于未加注的Kalman滤波器,但是在迭代中实现梯度下降方法,使得线性模型的参数在飞行期间可调。 通过引入观察噪声来抑制由神经模型过度装备问题引起的噪声。

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