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Adaptive Estimation of Multiple Fading Factors for GPS/INS Integrated Navigation Systems

机译:GPS / INS组合导航系统的多衰落因子自适应估计

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摘要

The Kalman filter has been widely applied in the field of dynamic navigation and positioning. However, its performance will be degraded in the presence of significant model errors and uncertain interferences. In the literature, the fading filter was proposed to control the influences of the model errors, and the H-infinity filter can be adopted to address the uncertainties by minimizing the estimation error in the worst case. In this paper, a new multiple fading factor, suitable for the Global Positioning System (GPS) and the Inertial Navigation System (INS) integrated navigation system, is proposed based on the optimization of the filter, and a comprehensive filtering algorithm is constructed by integrating the advantages of the H-infinity filter and the proposed multiple fading filter. Measurement data of the GPS/INS integrated navigation system are collected under actual conditions. Stability and robustness of the proposed filtering algorithm are tested with various experiments and contrastive analysis are performed with the measurement data. Results demonstrate that both the filter divergence and the influences of outliers are restrained effectively with the proposed filtering algorithm, and precision of the filtering results are improved simultaneously.
机译:卡尔曼滤波器已广泛应用于动态导航和定位领域。但是,如果存在重大的模型误差和不确定的干扰,其性能将下降。在文献中,提出了衰落滤波器来控制模型误差的影响,并且在最坏情况下可以通过使估计误差最小化来采用H-∞滤波器来解决不确定性。本文在优化滤波器的基础上,提出了一种适用于全球定位系统(GPS)和惯性导航系统(INS)组合导航系统的新的多衰落因子,并通过综合构建一种综合的滤波算法。 H无限滤波器和拟议的多重衰落滤波器的优点。 GPS / INS集成导航系统的测量数据是在实际条件下收集的。通过各种实验测试了所提出的滤波算法的稳定性和鲁棒性,并对测量数据进行了对比分析。结果表明,所提出的滤波算法有效地抑制了滤波散度和离群值的影响,同时提高了滤波结果的精度。

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