Integrity for Future SBAS Users: Concept and Experimentations

Odile Maliet, Julie Antic, Sébastien Trilles, Marie Abbal, Hélène Delfour-Cormier, Mickael Dall’Orso, Nicolas Giron, Guillaume Buscaret, Frédéric Bauert, Carlos Lopez de Echazarreta
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This improved positioning service should address both the SBAS ability to broadcast highly accurate corrections and reliable integrity data, as well as the user algorithm formulation which uses these SBAS products. Moreover, these users may evolve in environments not favorable to the correct reception of GNSS signals, implying possibly a fusion with measurements coming from other sensors. In this context, the use of Kalman filtering and hybridization with non-GNSS sensors seem highly recommended. For users implementing Kalman filtering, the knowledge of the time correlation of the GNSS measurements errors is of importance to determine correct overbounding models. The current MOPS integrity concept is not adapted for such new user solutions. Typically, CDF overbounding is applicable only for GNSS measurements with residual errors not correlated with time. 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In this experimentation, we consider Kalman filtering positioning using ionospheric free combination. We consider both a code only and a phase-based formulation (float ambiguity resolution). 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引用次数: 0

Abstract

The present paper summarizes the work carried out under the European H2020 R&D study “EGNOS Next System Feasibility study” for which a dedicated activity addresses a new integrity concept focused on the SBAS’ products in the pseudorange domain and aimed at new potential SoL users beyond the civil aviation user compliant to RTCA/EUROCAE MOPS [1], [2]. In GNSS applications, integrity is defined as a measure of the level of trust a user can place in a position estimate [3]. Th e classical Satellite Based Augmentation Systems (SBAS) aviation integrity concept relies on a stringent specification of the user algorithm implementation, described in the annex of the Minimum Operational Performance Standard (MOPS) [1], [2]. Similarly, again according to MOPS, current SBAS integrity data assumes that residual errors from broadcast corrections (satellite orbit/clock and ionosphere delays) are overbounded by a Gaussian Cumulative Distribution Function (CDF). For possible future SBAS’ applications such as maritime, rail, automotive and Unmanned Aerial Vehicle (UAV), the ability to provide tight and reliable protection volumes will be a critical enabler. To meet this level of performance, users will need to use more accurate positioning algorithms than the one specified in the MOPS for aviation users. This improved positioning service should address both the SBAS ability to broadcast highly accurate corrections and reliable integrity data, as well as the user algorithm formulation which uses these SBAS products. Moreover, these users may evolve in environments not favorable to the correct reception of GNSS signals, implying possibly a fusion with measurements coming from other sensors. In this context, the use of Kalman filtering and hybridization with non-GNSS sensors seem highly recommended. For users implementing Kalman filtering, the knowledge of the time correlation of the GNSS measurements errors is of importance to determine correct overbounding models. The current MOPS integrity concept is not adapted for such new user solutions. Typically, CDF overbounding is applicable only for GNSS measurements with residual errors not correlated with time. To cope with time correlation, recent developments introduce overbounding models of the Power Spectral Density (PSD) of the GNSS measurements residual errors[7]. In this paper we describe a new potential SBAS service which provides integrity parameters for a wide class of user algorithms. The new concept focuses on the integrity of SBAS products at pseudorange level to stay as much user agnostic as it can be, in the sense that it is demonstrated that these products are compatible with several user design solutions (variety of GNSS pre-correlation filters, variety of positioning algorithm formulations, several environments and user characteristics, etc…) and target integrity risks. For instance, these products are compatible with a Kalman filter using only code measurements and either the ionosphere -free combination or uncombined measurements, in a float ambiguity PPP Kalman filter with uncombined or ionosphere-free measurements. It combines the classical SBAS sigma parameters with PSD overbounding to enable its use by users implementing Kalman filtering. This concept consists in a combination of offline parameters and parameters estimated in real time. The offline parameters are checked by the system to confirm that the required assumptions for maintaining integrity remain verified, and can be updated by a command if needed. In addition, the SBAS navigation kernel supporting this service will implement precise orbit, clock, code, and phase bias computation for providing to the users the set of corrections compatible with Precise Point Positioning. The new potential service has been implemented in a System Test Bed that takes real measurements from IGS stations as inputs. The IGS network was chosen to mimic EGNOS and Galileo ground station networks. The integrity concept and its applicability were tested in an end-to-end experiment with real user data. In this experimentation, we consider Kalman filtering positioning using ionospheric free combination. We consider both a code only and a phase-based formulation (float ambiguity resolution). We demonstrate that the computed protection volumes are firstly reliable bounds of the position errors, and secondly compatible for more stringent applications querying smaller protection volumes.
未来SBAS用户的诚信:概念与实验
本文总结了在欧洲H2020研发研究“EGNOS下一个系统可行性研究”下开展的工作,其中一个专门的活动解决了一个新的完整性概念,重点关注SBAS在伪橙域的产品,并针对符合RTCA/EUROCAE MOPS的民用航空用户以外的新的潜在SoL用户[1],[2]。在GNSS应用中,完整性被定义为用户对位置估计的信任程度的度量[3]。经典的基于卫星的增强系统(SBAS)航空完整性概念依赖于用户算法实现的严格规范,在最低操作性能标准(MOPS)的附件中进行了描述[1],[2]。同样,根据MOPS,当前SBAS完整性数据假设广播校正(卫星轨道/时钟和电离层延迟)的残余误差被高斯累积分布函数(CDF)超越。对于未来可能的SBAS应用,如海事、铁路、汽车和无人机(UAV),提供紧密可靠的保护容量的能力将是关键的推动因素。为了达到这一性能水平,用户将需要使用比MOPS中为航空用户指定的更精确的定位算法。这种改进的定位服务应该解决SBAS广播高精度校正和可靠完整性数据的能力,以及使用这些SBAS产品的用户算法制定。此外,这些用户可能在不利于正确接收GNSS信号的环境中进化,这意味着可能会与来自其他传感器的测量结果融合。在这种情况下,强烈建议使用卡尔曼滤波和非gnss传感器的杂交。对于实现卡尔曼滤波的用户来说,了解GNSS测量误差的时间相关性对于确定正确的过界模型非常重要。当前的MOPS完整性概念不适用于这种新的用户解决方案。一般来说,CDF过限只适用于残差与时间不相关的GNSS测量。为了处理时间相关性,最近的发展引入了GNSS测量剩余误差的功率谱密度(PSD)的过边界模型[7]。在本文中,我们描述了一种新的潜在的SBAS服务,它为广泛的用户算法提供了完整性参数。新概念侧重于伪距离水平的SBAS产品的完整性,以尽可能保持与用户无关,从某种意义上说,这些产品兼容多种用户设计解决方案(各种GNSS预相关滤波器、各种定位算法配方、几种环境和用户特征等)和目标完整性风险。例如,这些产品与仅使用代码测量和无电离层组合或未组合测量的卡尔曼滤波器兼容,在浮动模糊PPP卡尔曼滤波器中具有无组合或无电离层测量。它将经典的SBAS sigma参数与PSD过限相结合,使其能够被实现卡尔曼滤波的用户使用。这个概念包括离线参数和实时估计参数的结合。离线参数由系统检查,以确认维护完整性所需的假设仍然得到验证,如果需要,可以通过命令更新。此外,支持该服务的SBAS导航内核将实现精确的轨道、时钟、代码和相位偏差计算,为用户提供与精确点定位兼容的校正集。新的潜在服务已经在一个系统测试台中实现,该测试台将IGS站点的实际测量作为输入。IGS网络被选择用来模拟EGNOS和伽利略地面站网络。通过端到端真实用户数据实验,验证了完整性概念及其适用性。在本实验中,我们考虑利用电离层自由组合进行卡尔曼滤波定位。我们考虑了仅代码和基于相位的公式(浮点模糊解决)。我们证明计算的保护体积首先是位置误差的可靠边界,其次兼容更严格的应用,查询更小的保护体积。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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