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An Improved Strong Tracking Cubature Kalman Filter for GPS/INS Integrated Navigation Systems

机译:用于GPS / INS组合导航系统的改进型强跟踪Cubature卡尔曼滤波器

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摘要

The cubature Kalman filter (CKF) is widely used in the application of GPS/INS integrated navigation systems. However, its performance may decline in accuracy and even diverge in the presence of process uncertainties. To solve the problem, a new algorithm named improved strong tracking seventh-degree spherical simplex-radial cubature Kalman filter (IST-7thSSRCKF) is proposed in this paper. In the proposed algorithm, the effect of process uncertainty is mitigated by using the improved strong tracking Kalman filter technique, in which the hypothesis testing method is adopted to identify the process uncertainty and the prior state estimate covariance in the CKF is further modified online according to the change in vehicle dynamics. In addition, a new seventh-degree spherical simplex-radial rule is employed to further improve the estimation accuracy of the strong tracking cubature Kalman filter. In this way, the proposed comprehensive algorithm integrates the advantage of 7thSSRCKF’s high accuracy and strong tracking filter’s strong robustness against process uncertainties. The GPS/INS integrated navigation problem with significant dynamic model errors is utilized to validate the performance of proposed IST-7thSSRCKF. Results demonstrate that the improved strong tracking cubature Kalman filter can achieve higher accuracy than the existing CKF and ST-CKF, and is more robust for the GPS/INS integrated navigation system.
机译:卡尔曼滤波器(CKF)被广泛用于GPS / INS集成导航系统的应用中。但是,其性能可能会降低准确性,甚至在存在过程不确定性的情况下也可能会有所不同。为解决这一问题,本文提出了一种新的算法,称为改进的强跟踪七度球面单形-径向孔格卡尔曼滤波器(IST-7thSSRCKF)。该算法采用改进的强跟踪卡尔曼滤波技术减轻了工艺不确定性的影响,采用假设检验的方法识别工艺不确定性,并根据在线修改了CKF中的先验状态估计协方差。车辆动力学的变化。另外,采用了新的七度球面单纯形-径向法则来进一步提高强跟踪库尔曼卡尔曼滤波器的估计精度。这样,拟议的综合算法将7thSSRCKF的高精度与强大的跟踪滤波器的强大鲁棒性相结合,克服了过程不确定性。具有明显动态模型误差的GPS / INS集成导航问题被用来验证所提出的IST-7thSSRCKF的性能。结果表明,改进的强跟踪库尔曼滤波器比现有的CKF和ST-CKF可以获得更高的精度,并且对于GPS / INS集成导航系统更强大。

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