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The Optimal Degree of Gravity Spherical Harmonic Model Calculation for Gravity Disturbance Compensation in Inertial Navigation

机译:惯性导航中重力干扰补偿的最佳重力球谐模型计算

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In recent years, the significant improvement of inertial navigation, leaves the gravity disturbance as the important factor which affects the accuracy of inertial navigation. This paper focus on the compensation for gravity disturbance with gravity spherical harmonic model, especially the optimal degree of gravity spherical harmonic model with which to calculate the gravity disturbance. The effect of gravity disturbance on inertial navigation is analysed based on the amplitude-frequency response characteristics of inertial navigation error differential equation, then the dominantly influential frequency band of gravity disturbance can be found which is the target of compensation. Combination the dominantly influential frequency band with the spatial resolution of the Earth’s gravity spherical harmonic model EGM2008 which is used to calculate the gravity disturbance, the optimal degree can be determined based on an algorithm proposed in this paper. Finally, shipborne inertial navigation experiment confirms the correctness and effectiveness of the proposed algorithm.
机译:近年来,惯性导航的重大改进,使重力扰动成为影响惯性导航精度的重要因素。本文着重于利用重力球谐模型对重力扰动进行补偿,尤其是用于计算重力扰动的最佳重力球谐模型。根据惯性导航误差微分方程的幅频响应特性,分析了重力扰动对惯性导航的影响,可以找到重力扰动的主要影响频段,作为补偿的目标。将主要影响频段与用于计算重力扰动的地球重力球谐模型EGM2008的空间分辨率相结合,可以基于本文提出的算法确定最佳程度。最后,舰载惯性导航实验验证了所提算法的正确性和有效性。

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