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Comparison on H∞ Filter and Kalman Filter for Initial Alignment of SINS on Static Base

机译:H∞滤波器和卡尔曼滤波器的比较静态基地循环初始对齐

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This paper discusses two kinds of initial alignment for Strap-down Inertial Navigation System (SINS), one is based on Kalman filter, and the other is based on H∞ filter. Through modeling, simulating and comparing, it can be concluded that using the former, with given system model and the noise characteristics, the leveling misalignment angles converge relatively rapid, but the azimuth misalignment angle converges relatively slow. If there is too large disturbance on system model, Kalman filter would be prolonged, even be emanated. However, the standard Kalman filter performances can be improved by using H∞ filter. The latter performs better than the former in azimuth alignment and equivalent to the former in level alignment. And H∞ filter can also greatly enhances the robustness of the system. So H∞ filter is an available method for the initial alignment.
机译:本文讨论了用于带下惯性导航系统(SINS)的两种初始对准,是基于卡尔曼滤波器,另一个基于H∞滤波器。通过建模,模拟和比较,可以得出结论,使用前者,具有给定系统模型和噪声特性,平整的未对准角度会聚相对较快,但方位角错位角会聚相对较慢。如果对系统模型过大的干扰太大,卡尔曼滤波器将延长,甚至会被散发。但是,通过使用H∞过滤器可以提高标准的卡尔曼滤波器性能。后者在方位角对齐方面比以前更好地执行,并且等同于前者在水平对齐中。 H∞过滤器也可以大大提高系统的鲁棒性。因此,H∞过滤器是初始对齐的可用方法。

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