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Damping strapdown inertial navigation system based on a Kalman filter

机译:基于卡尔曼滤波器的阻尼捷联惯性导航系统

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摘要

A damping strapdown inertial navigation system (DSINS) can effectively suppress oscillation errors of strapdown inertial navigation systems (SINSs) and improve the navigation accuracy of SINSs. Aiming at overcoming the disadvantages of traditional damping methods, a DSINS, based on a Kalman filter (KF), is proposed in this paper. Using the measurement data of accelerometers and calculated navigation parameters during the navigation process, the expression of the observation equation is derived. The calculation process of the observation in both the internal damping state and the external damping state is presented. Finally, system oscillation errors are compensated by a KF. Simulation and test results show that, compared with traditional damping methods, the proposed method can reduce system overshoot errors and shorten the convergence time of oscillation errors effectively.
机译:阻尼捷联惯性导航系统(DSINS)可以有效抑制捷联惯性导航系统(SINSs)的振荡误差,提高捷联惯导系统的导航精度。为了克服传统阻尼方法的弊端,提出了一种基于卡尔曼滤波器(KF)的DSINS。在导航过程中,使用加速度计的测量数据和计算出的导航参数,得出观测方程的表达式。给出了内部阻尼状态和外部阻尼状态下观测值的计算过程。最后,系统振荡误差由KF补偿。仿真和测试结果表明,与传统的阻尼方法相比,该方法可以减少系统过冲误差,并有效缩短振荡误差的收敛时间。

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