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Self-Gradient Compensation of Full-Tensor Airborne Gravity Gradiometer

机译:全张量机载重力梯度仪的自梯度补偿

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摘要

In the process of airborne gravity gradiometry for the full-tensor airborne gravity gradiometer (FTAGG), the attitude of the carrier and the fuel mass will seriously affect the accuracy of gravity gradiometry. A self-gradient is the gravity gradient produced by the surrounding masses, and the surrounding masses include distribution mass for the carrier mass and fuel mass. In this paper, in order to improve the accuracy of airborne gravity gradiometry, a self-gradient compensation model is proposed for FTAGG. The self-gradient compensation model is a fuction of attitude for carrier and time, and it includes parameters ralated to the distribution mass for the carrier. The influence of carrier attitude and fuel mass on the self-gradient are simulated and analyzed. Simulation shows that the self-gradient tensor element Γxx,Γxy,Γxz,Γyz and Γzz are greatly affected by the middle part of the carrier, and the self-gradient tensor element Γyz is affected by the carrier’s fuel mass in three attitudes. Further simulation experiments show that the presented self-gradient compensation method is valid, and the error of the self-gradient compensation is within 0.1 Eu. Furthermore, this method can provide an important reference for improving the accuracy of aviation gravity gradiometry.
机译:在全张量机载重力梯度仪(FTAGG)的机载重力梯度仪过程中,载体的姿态和燃料质量会严重影响重力梯度仪的精度。自梯度是由周围质量产生的重力梯度,周围质量包括载体质量和燃料质量的分布质量。为了提高机载重力梯度仪的精度,提出了一种针对FTAGG的自梯度补偿模型。自梯度补偿模型是对载体和时间的态度的函数,它包括与载体的分布质量相关的参数。模拟和分析了载架姿态和燃料质量对自梯度的影响。仿真表明,自梯度张量元素 < msub> Γ x x Γ x y Γ x z Γ y z < / msub> Γ z z 受载体中间部分和自梯度张量元素 Γ y z 受t影响他的载具的燃油质量有三种态度。进一步的仿真实验表明,所提出的自梯度补偿方法是有效的,自梯度补偿的误差在0.1 Eu以内。此外,该方法可为提高航空重力梯度仪的精度提供重要参考。

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