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Integrity Monitoring Algorithms using Filtering Approaches for Higher Navigation Performance: Consideration of the non-Gaussian GNSS Measurements

机译:完整性监控算法使用过滤方法进行较高导航性能:考虑非高斯GNSS测量

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For safety-critical applications of global navigation satellite systems (GNSS), such as aviation and missile navigation systems, it is important to detect and exclude faults that cause accuracy and integrity risks, so that the navigation system can operate continuously without performance degradation. For high accurate systems, the integrity monitoring function needs to detect and exclude small biases. And as more independent GNSSs (ex. GALILEO and GLONASS) are being available, we need to take into account simultaneous faults of multiple satellites. It also estimates protection level that determines availability of the navigation system. With conventional snapshot RAIM algorithms, it is difficult to detect small errors and simultaneous multiple faults. Assumed that we know the system dynamics, filtering algorithms, such as the Kalman filter, can provide better monitoring performance than the snapshot algorithms can, because the filter reduces noise level of measurements. However, because the Kalman filter presumes that measurement noise and disturbance follow the Gaussian distribution, its performance might degrades if the assumption is not right. To address this problem, we propose a fault detection and exclusion algorithm using particle filters. The particle filters are popular filtering methods to estimate states of a general dynamic system. It can deal with any system nonlinearities or any noise distributions using sequential Monte Carlo method, and present the posterior distributions of the states completely. Because GNSS measurement noise does not follow the Gaussian distribution perfectly, the particle filter can estimate the posterior distribution more accurately; therefore it has better integrity monitoring performance. Also, if the system has high non-linearity, the performance is getting better. Additionally, an integrity monitoring algorithm using the Gaussian Sum Filter is proposed as an alternative to the particle filter method that needs high computational load. The paper describes the detailed algorithms, and shows simulation and experiment results to evaluate integrity monitoring performance of the algorithms. The proposed algorithms detect 20% smaller faults and generate 30% lower protection levels than the conventional filtering methods that use the overbounded sigmas considering the non-Gaussian measurement distribution can. The results show that the proposed algorithms that do not use the overbounding method can provide better accuracy and availability performance just by changing the filtering algorithm.
机译:对于全球导航卫星系统(GNSS)安全关键型应用,如航空和导弹导航系统,它来检测和排除故障是造成准确性和完整性的风险,从而使导航系统能够连续而不会降低性能操作是很重要的。对于高精确的系统,完整性监控功能需要检测和排除小的偏差。随着越来越多的独立的GNSS(例如伽利略和GLONASS)都可用,我们需要考虑到多颗卫星的帐户同时故障。它还估计,决定了导航系统的可用性保护级别。与传统的快照RAIM算法,它是难以检测的小误差和同时多故障。假设我们知道系统动力学,过滤算法,如卡尔曼滤波器,可提供比快照算法更好的监控性能就可以了,因为过滤器减少测量噪音水平。然而,由于卡尔曼滤波器假定测量噪声和干扰遵循高斯分布,其性能可能降级,如果假设是不正确的。为了解决这个问题,我们提出了故障检测和使用的粒子滤波算法排除。所述颗粒过滤器是流行的过滤方法来估计一个一般的动态系统的状态。它可以处理任何系统非线性或使用连续的蒙特卡洛方法的任何噪声分布,而完全呈现状态的后验分布。因为GNSS测量噪声不遵循高斯分布完美,颗粒过滤器可以更准确地估计的后验分布;因此它具有更好的完整性监测性能。此外,如果系统具有较高的非线性,性能越来越好。另外,利用高斯累加滤波器的完整性监视算法作为替代,需要高计算负载的颗粒过滤器的方法。本文介绍了详细的算法,并显示仿真和实验结果来评估的算法完整性监视性能。所提出的算法检测小20%的故障和产生比使用考虑到非高斯分布测量罐中的overbounded西格玛常规过滤方法低30%的保护水平。结果表明,不使用的超限方法所提出的算法可以只通过改变滤波算法提供更好的精度和可用性性能。

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