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arXiv 2103.10696eess.SYcs.SY
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紧耦合GNSS/INS导航系统中的鲁棒状态与保护级估计

Robust state and protection-level estimation within tightly coupled GNSS/INS navigation system

Shuchen Liu, Kaizheng Wang, Dirk Abel

AI总结:

针对城市环境中GNSS信号干扰影响导航状态估计与保护级生成的问题,提出融合扩展H∞滤波器鲁棒状态估计与zonotope保护级计算的紧耦合GNSS/INS导航方案,经实测验证精度、鲁棒性更优且可实时应用。

摘要:

在交通出行类自主应用中,车辆状态的高速率、高精度估计通过融合全球导航卫星系统(GNSS)与惯性传感器的测量值实现。城市环境中的卫星信号干扰,以及由此导致的卫星观测值参数化效果不佳,往往会影响状态估计及其保护级生成的性能。为此,我们提出了一种创新方案,采用扩展H∞滤波器(EHF)实现鲁棒状态估计,并使用zonotope(zonotope,多面体 zonotope)生成保护级。该方案是基于惯性导航系统、由GPS/Galileo双星座卫星导航系统辅助的紧耦合导航系统的组成部分,具体采用了GNSS伪距和Δ距观测值。对真实世界数据集进行后处理的实验结果表明,在多种GNSS测量参数化方式和环境条件下,EHF在导航精度与鲁棒性方面相较传统扩展卡尔曼滤波器具有显著优势。基于zonotope的保护级计算被验证是有效的,计算成本可控,且具备实时实现的可行性。

英文摘要:

In autonomous applications for mobility and transport, a high-rate and highly accurate vehicle-state estimation is achieved by fusing measurements of global navigation satellite systems (GNSS) and inertial sensors. The state estimation and its protection-level generation often suffer from satellite-signal disturbances in urban environments and subsequent poor parametrization of the satellite observables. Thus, we propose an innovative scheme involving an extended H_infinity filter (EHF) for robust state estimation and zonotope for the protection-level generation. This scheme is shown as part of a tightly coupled navigation system based on an inertial navigation system and aided by the GPS/Galileo dual-constellation satellite navigation system. Specifically, GNSS pseudorange and deltarange observables are utilized. The experimental results of post-processing a real-world dataset show significant advantages of EHF against a conventional extended Kalman filter regarding the navigation accuracy and robustness under various GNSS-measurement parametrizations and environmental circumstances. The zonotope-based protection-level calculation is proven valid, computationally affordable, and feasible for real-time implementations.

机构、总结、中文摘要均由AI分析而来,可能存在错误,请以论文正文为准。

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