GNSS定位的完整性约束因子图优化

Xiao Xia, L. Hsu, W. Wen
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引用次数: 0

摘要

全球导航卫星系统(GNSS)完整性的概念是指对GNSS定位解决方案的信任度量,这对于航空和自动驾驶等安全关键应用至关重要。虽然完整性监测最早被引入并广泛应用于GNSS航空领域,但由于卫星能见度有限、多径强、非视距(NLOS)效应等特殊情况,完整性监测并不适用于城市场景的GNSS定位。例如,直接排除GNSS多路径和NLOS会显著降低几何约束,从而导致高度保守的完整性监测(IM)。因此,在城市峡谷中,有限的GNSS测量冗余和不确定度建模不准确将严重降低GNSS定位和完整性监测的性能。为了解决这些问题,本文提出了一种基于可切换约束的完整性约束因子图优化(FGO)方法。与传统GNSS IM方法考虑单历元或两个连续历元测量相比,该方法通过因子图结构提高了测量冗余度。同时,通过可切换约束引入的开关变量与每个伪距测量相连接,既能估计测量不确定性,又能在保持卫星几何形状的前提下满足常规故障检测与排除(FDE)的卡方检验。特别是,计算的保护等级考虑了开关变量的影响,从而更准确地约束了位置误差。在带有高斯随机噪声的开放天空数据集上对该方法的性能进行了评估。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Integrity-constrained Factor Graph Optimization for GNSS Positioning
The concept of global navigation satellite system (GNSS) integrity refers to the measure of trust of the GNSS positioning solution, which is vital for safety-critical applications such as aviation and autonomous driving. While integrity monitoring was firstly introduced and widely applied in the GNSS aviation field, it is not suitable for GNSS positioning in urban scenarios due to unique circumstances such as limited satellite visibility, strong multipath and non-line-of-sight (NLOS) effects. For example, the direct exclusion of the GNSS multipath and NLOS would significantly degrade the geometry constraints, thus leading to highly conservative integrity monitoring (IM). As a result, the limited GNSS measurement redundancy and the inaccurate measurement uncertainty modeling in urban canyons will severely degrade the performance of both the GNSS positioning and integrity monitoring. To alleviate these issues, this paper proposed an integrity-constrained factor graph optimization (FGO) for GNSS positioning with the help of switchable constraints. Compared to the conventional GNSS IM methods which consider measurements in single epoch or two successive epochs, the proposed method improves the measurement redundancy by the factor graph structure. Meanwhile, the switch variable, which is introduced by switchable constraints and connected with each pseudorange measurement, can not only estimate the measurement uncertainties, but also satisfying the Chi-square testing of the conventional fault detection and exclusion (FDE) while maintaining satellite geometry. In particular, the calculated protection levels consider the effect of switch variables, hence bound the position error more accurately. The performance of this proposed method is evaluated on open-sky dataset with manually injected biases with gaussian random noise.
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