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The study of Kalman filtering algorithm in the initial alignment of strapdown inertial navigation system

机译:卡尔曼滤波算法在初始对准中的初始惯性导航系统中的研究

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According to the principle and the method of initial alignment of strapdown inertial navigation system, proposed based on Sage-Husa adaptive kalman filter algorithm. The measured simulation data, compared with those of kalman filtering algorithm, show that the optimized algorithm can optimize the noise estimation, revise accumulated error of strapdown inertial navigation system, and greatly improve the navigation accuracy.
机译:根据STAPDOWN惯性导航系统初始对准的原理和方法,提出基于SAGE-HUSA自适应卡尔曼滤波算法。与卡尔曼滤波算法相比,测量的仿真数据,表明优化算法可以优化噪声估计,修改截头惯性导航系统的累计误差,大大提高了导航精度。

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