Aeromagnetic attitude compensation for uninhabited aircraft systems without high-altitude calibration patterns using hybrid recurrent neural networks

Q2 Earth and Planetary Sciences Leading Edge Pub Date : 2023-02-01 DOI:10.1190/tle42020112.1
M. Cunningham, L. Tuck, C. Samson, J. Laliberté, M. Goldie, Alan Wood, David Birkett
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Abstract

Since the 1950s, Tolles-Lawson-based aeromagnetic compensation methods have been used to separate an aircraft's magnetic signal from signal associated with ground geologic and cultural features. This is done by performing a high-altitude figure-of-merit (FOM) flight and fitting the band-pass-filtered magnetic data to determine compensation parameters. This paper describes a supervised hybrid recurrent neural network (HRNN) algorithm trained on low-altitude survey data to perform aeromagnetic compensation. The proposed HRNN attitude compensation method can be employed for aeromagnetic surveys where traditional FOM and compensation are not possible. It has particular relevance for surveying via uninhabited aircraft systems (UAS). Firstly, the HRNN was tested on data from a fixed-wing airplane survey, and the results were compared to hardware-based compensation results. The standard deviation of the difference between the two methods for magnetic attitude correction (MAC) was 0.1 nT for the training region and 0.4 nT for the application region, respectively. Secondly, a UAS FOM flight at the highest permitted altitude in Canada, 120 m above ground level, showed similar improvement ratios for software-based least squares (LS) and the proposed HRNN algorithm of 3.5 and 2.6, respectively. The percent change and deviation in differences in MACs from LS to HRNN was 0.0% and 0.9 nT across small-box loops and –2.7% and 0.4 nT across large-box loops. Finally, LS and the proposed HRNN algorithm were applied to a 50 m altitude UAS data set for which no FOM flight was possible. LS did not successfully model aircraft noise, whereas the HRNN demonstrated effective removal of the magnetic signal due to aircraft attitude variations. The modeled HRNN MAC had a standard deviation of 2.4 nT.
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基于混合递归神经网络的无高空定标无人飞行器系统航磁姿态补偿
自20世纪50年代以来,基于tolles - lawson的航空磁补偿方法已被用于将飞机的磁信号与与地面地质和文化特征相关的信号分离开来。这是通过执行高空性能图(FOM)飞行和拟合带通滤波磁数据来确定补偿参数来完成的。本文提出了一种基于低空测量数据训练的有监督混合递归神经网络(HRNN)算法进行航磁补偿。所提出的HRNN姿态补偿方法可用于航磁测量中无法进行传统形式补偿的情况。它特别适用于通过无人驾驶飞机系统(UAS)进行测量。首先,在固定翼飞机调查数据上对HRNN进行了测试,并与基于硬件的补偿结果进行了比较。两种磁姿态校正方法在训练区和应用区差异的标准差分别为0.1 nT和0.4 nT。其次,在加拿大最高允许高度120 m的UAS FOM飞行中,基于软件的最小二乘(LS)和提出的HRNN算法的改进率相似,分别为3.5和2.6。从LS到HRNN的mac差异的百分比变化和偏差在小盒环中为0.0%和0.9 nT,在大盒环中为-2.7%和0.4 nT。最后,将LS和提出的HRNN算法应用于50 m高度不可能进行FOM飞行的UAS数据集。LS没有成功地模拟飞机噪声,而HRNN证明了由于飞机姿态变化引起的磁信号的有效去除。模型HRNN MAC的标准差为2.4 nT。
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来源期刊
Leading Edge
Leading Edge Earth and Planetary Sciences-Geology
CiteScore
3.10
自引率
0.00%
发文量
180
期刊介绍: THE LEADING EDGE complements GEOPHYSICS, SEG"s peer-reviewed publication long unrivalled as the world"s most respected vehicle for dissemination of developments in exploration and development geophysics. TLE is a gateway publication, introducing new geophysical theory, instrumentation, and established practices to scientists in a wide range of geoscience disciplines. Most material is presented in a semitechnical manner that minimizes mathematical theory and emphasizes practical applications. TLE also serves as SEG"s publication venue for official society business.
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