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A novel application of adaptive filtering for initial alignment of Strapdown Inertial Navigation System

机译:自适应滤波在捷联惯导系统初始对准中的新应用

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摘要

A novel method for improving the alignment accuracy and convergence speed of strap down inertial navigation system has been reported in this paper. From the dynamic model, the Strapdown Inertial Navigation System (SINS) error model is derived for a small misalignment angle. Many algorithms are proposed for proper estimation of alignment accuracy for INS. Keeping this view in mind we propose two novel algorithms viz. Volterra Recursive Least Square (VRLS) and Bilinear Recursive Least Square (BRLS) based on nonlinear adaptive filter for the estimation of accurate azimuth alignment error. The comparative performances of the aforesaid algorithms are presented to show the effectiveness of the proposed (BRLS) algorithm. The effective performance of proposed BRLS algorithm in presence of three different white Gaussian noise with is studied for the first time in MATLAB simulating environment. The comparative analysis is precisely presented to realize the validation of proposed BRLS algorithm which is compared with recently proposed Kalman filter and Sage-Husa algorithms. The proposed BRLS algorithm enhances the convergence rate of azimuth attitude error and alignment accuracy effectively.
机译:本文报道了一种提高捷联惯性导航系统对准精度和收敛速度的新方法。从动态模型中,可以得出针对小失准角的捷联惯性导航系统(SINS)误差模型。为了正确估计INS的对准精度,提出了许多算法。牢记这一观点,我们提出了两种新颖的算法。基于非线性自适应滤波器的Volterra递归最小二乘(VRLS)和双线性递归最小二乘(BRLS)用于估计精确的方位对准误差。给出了上述算法的比较性能,以证明所提出算法的有效性。在MATLAB仿真环境中,首次研究了所提出的BRLS算法在三种不同的高斯白噪声存在下的有效性能。精确地进行了比较分析,以实现所提出的BRLS算法的验证,并将其与最近提出的Kalman滤波器和Sage-Husa算法进行比较。提出的BRLS算法有效地提高了方位角误差的收敛速度和对准精度。

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