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New Strapdown Airborne Gravimetry Algorithms: Testing with Real Flight Data

机译:新的挂机机载重力算法:使用真正的飞行数据进行测试

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The paper presents new algorithms for strapdown airborne gravimetry and the results of processing real data from a survey flight carried out by DTU Space, Denmark, in 2019 using an iMAR system. The developed algorithms cover all stages of airborne data postprocessing, namely: computing GNSS solutions, initial alignment of gravime-ter's inertial measurement unit (IMU), IMU-GNSS integration, and gravity estimation. At the latter, we solve two different problems, one of which is esti-mation of only the vertical component of the gravity vector (scalar gravimetry) and the other is estimation of all three gravity vector components (vector gravimetry). The scalar gravimetry algorithm is based on modeling gravity in time and Kalman filtering. The accuracy of the gravity estimates obtained from processing the iMAR flight data is 1.1 mGal (RMS) based on the cross-over analysis (for the filter cutoff frequency of 1/100 Hz). The vector gravimetry algorithm is based on spatial gravity modeling and using the Kalman filter in the information form. The accuracy of the gravity horizontal component estimates was evaluated by comparison with EGM2008 and equals 2 mGal (STD), which can be regarded as a promising result for airborne vector gravimetry.
机译:本文介绍了拟计空气传播重食的新算法,以及由DTU空间,丹麦的调查飞行处理实际数据的结果,2019年使用IMAR系统。开发的算法涵盖了后处理的所有空气数据阶段,即:计算GNSS解决方案,初始对准骨骼惯性测量单元(IMU),IMU-GNSS集成和重力估计。在后者,我们解决了两个不同的问题,其中一个是只有重力矢量(标量重量法)的垂直分量,另一个是估计所有三个重力矢量分量(矢量重量法)。标量重量算法基于时间和卡尔曼滤波的重力建模。根据交叉分析(对于1/100Hz的滤波器截止频率),从处理IMAR飞行数据获得的重力估计的准确性为1.1 mgal(RMS)。载体重量算法基于空间重力建模,并在信息形式中使用卡尔曼滤波器。通过与EGM2008进行比较来评估重力水平分量估计的精度,并且等于2mgal(STD),其可以被认为是空气传播载体重量的有希望的结果。

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