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Proceedings of the ION 2019 Pacific PNT Meeting最新文献

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Future of Space-based PNT 天基PNT的未来
Pub Date : 2019-04-11 DOI: 10.33012/2019.16792
David C. Chapman
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引用次数: 0
Assessment and Mitigation of Ionospheric Spatial Decorrelation on GBAS: Lessons Learned GBAS上电离层空间去相关的评估和缓解:经验教训
Pub Date : 2019-04-11 DOI: 10.33012/2019.16840
Jiyun Lee
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引用次数: 0
Revaluation of Spatial Decorrelation Parameters of Atmospheric Delay for GBAS (Ground-based Augmentation System) Safety Design 地面增强系统安全设计中大气延迟空间去相关参数的重估
Pub Date : 2019-04-11 DOI: 10.33012/2019.16851
T. Yoshihara, S. Saito, A. Kezuka, S. Saitoh
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引用次数: 0
Barometer Assisted GPS Denied Trilateration Algorithm for Traversing Vertical Three-Dimensional Spaces 晴雨表辅助GPS拒绝三边测量算法在垂直三维空间中的应用
Pub Date : 2019-04-11 DOI: 10.33012/2019.16802
Alvin Goh Cheng Ann, Alvee Ahmed, G. Soh, S. Foong
GPS denied localization has increasing application for indoor tracking and navigation. However, general literature focus on finding a location solution within the horizontal x-y plane. We propose a GPS-denied localization algorithm that targets better accuracy for a user travelling significant vertical distances compared to level ground. This algorithm works on the basis of taking a height reading from a barometer and reducing the trilateration problem into a two-dimensional problem. With this algorithm, we are able to obtain a three-dimensional solution with less time and comparable accuracy to conventional three-dimensional trilateration. Our simulations and initial hardware testing show that utilizing the barometer’s readings could cut the computation time compared to conventional three-dimensional algorithms as measurement noise increases relative to the range measurements. We intend to apply the results of this study to an algorithm that can optimize node placement in three-dimensional space, all while the user travels through an area and plants new anchors for the localization network.
GPS拒绝定位在室内跟踪和导航中的应用越来越广泛。然而,一般文献集中于寻找水平x-y平面内的位置解。我们提出了一种gps拒绝定位算法,与平地相比,该算法的目标是为用户行驶显著的垂直距离提供更好的精度。该算法基于从气压计中获取高度读数,并将三边测量问题简化为二维问题。使用该算法,我们能够以更少的时间和与传统的三维三边测量相当的精度获得三维解。我们的模拟和初始硬件测试表明,与传统的三维算法相比,使用气压计的读数可以减少计算时间,因为测量噪声相对于测量范围增加。我们打算将这项研究的结果应用于一种算法,该算法可以在用户穿过一个区域并为定位网络植入新的锚点的同时,优化三维空间中的节点放置。
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引用次数: 2
Transfer Alignment Using Synergistic IMUs 使用协同imu的转移校准
Pub Date : 2019-04-11 DOI: 10.33012/2019.16775
S. Moafipoor, Brad Despres, J. Fayman, L. Bock
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引用次数: 0
Lower Bounds in Optimal Integrity Monitoring 最优完整性监控的下界
Pub Date : 2019-04-11 DOI: 10.33012/2019.16788
J. Blanch, T. Walter
The goal of integrity monitoring in positioning algorithms consists in finding a test statistic and an estimator that meets both the integrity requirements and the alert requirements under a set of conditions. The search for such test statistics can be cast as an optimization problem where the goal is to minimize the integrity risk while maintaining the alert requirements. In this work, we provide results that extend previous results in two ways. First, we provide a lower bound on the integrity risk for linear unbiased estimators (but not necessarily optimal). Second we provide a lower on the integrity risk in the case of fault detection and exclusion. The results developed in this work here are general. In particular, they are applicable to both snapshot solutions and Kalman filter solutions, and to any combination of sensors. INTRODUCTION Until recently, integrity monitoring in radio-navigation was mostly limited to aircraft navigation. It is now being expanded to automotive, rail, and maritime applications [1], [2], [3]. Given the increased awareness of GNSS threats (like spoofing), it is likely that integrity monitoring will pervade most navigation systems. There are many different types of integrity monitoring algorithms, each responding to a different design constraint. In all cases, it can be useful to know what the minimum achievable integrity risk is, for at least three reasons. First, these bounds tell us whether it makes sense to continue improving the algorithm; second, the search itself shows us which class of algorithms will likely perform well, third, if the lower limit is too high, then we know that we should be looking somewhere else to achieve the desired performances (like more measurements, additional structure, or more constraints on the fault modes). Finding the optimal integrity monitoring algorithm is in general a very difficult problem. It is however possible to define tractable problems that can be proven to provide a lower bound on the achievable integrity risk in the original problems. Optimality results in the range domain pre-date the development of integrity in GNSS ([4], [5]). These results have been adapted to GNSS in at least [6]. In [7], we proved that in the case of one threat, even multi-dimensional, the optimal detection statistic is the solution separation statistic. This was achieved by casting the search of the optimal detection region as a minimax problem, and using the Neyman-Pearson lemma to limit the search of the detection regions to a class of regions parameterized by a bias. These results allowed us to establish a lower bound on the minimum integrity risk. However, these results were only proven for least squares estimators and for the detection problem only. In this work, we expand and generalize the theoretical results from [7] in two directions. First, we provide lower bounds on the lowest possible achievable integrity risk given a set of measurements and a threat space in the case of linear esti
定位算法中完整性监测的目标在于找到在一定条件下既满足完整性要求又满足警报要求的测试统计量和估计量。搜索这样的测试统计信息可以看作是一个优化问题,其目标是在保持警报需求的同时最小化完整性风险。在这项工作中,我们以两种方式提供了扩展先前结果的结果。首先,我们提供了线性无偏估计的完整性风险的下界(但不一定是最优的)。其次,在故障检测和排除的情况下,我们提供了较低的完整性风险。在此工作中得出的结果是一般性的。特别是,它们既适用于快照解决方案,也适用于卡尔曼滤波解决方案,也适用于任何传感器组合。直到最近,无线电导航中的完整性监测主要局限于飞机导航。它现在正在扩展到汽车,铁路和海事应用[1],[2],[3]。鉴于对GNSS威胁(如欺骗)的认识不断提高,完整性监测很可能会渗透到大多数导航系统中。有许多不同类型的完整性监控算法,每一种都响应不同的设计约束。在所有情况下,了解可实现的最小完整性风险是什么是有用的,原因至少有三个。首先,这些界限告诉我们继续改进算法是否有意义;第二,搜索本身向我们展示了哪一类算法可能会表现良好,第三,如果下限太高,那么我们知道我们应该寻找其他地方来实现期望的性能(比如更多的测量,额外的结构,或者对故障模式的更多约束)。寻找最优的完整性监控算法通常是一个非常困难的问题。然而,可以定义可处理的问题,这些问题可以证明在原始问题中提供可实现的完整性风险的下界。距离域的最优性结果早于GNSS完整性的发展([4],[5])。这些结果至少在[6]中被用于GNSS。在[7]中,我们证明了在一个威胁甚至多维的情况下,最优检测统计量是解分离统计量。这是通过将最优检测区域的搜索转换为极小极大问题,并使用Neyman-Pearson引理将检测区域的搜索限制为一类由偏差参数化的区域来实现的。这些结果使我们能够建立最小完整性风险的下限。然而,这些结果只证明了最小二乘估计和检测问题。在这项工作中,我们从两个方向对[7]的理论结果进行了扩展和推广。首先,在线性估计(但不一定是最小二乘)的情况下,我们给出了给定一组测量值和威胁空间的最低可能实现完整性风险的下界;其次,我们将考虑使用非线性估计器进行故障检测和排除的情况。对于这种情况,我们将证明,为了获得最优结果,对故障检测和排除过程进行推广是有用的。在介绍了符号、定义和以前的结果之后,我们提供了两个不等式,在给定警报概率的情况下,对最优完整性给出了下界。误差模型与定义无故障误差模型在本文中,我们假设线性近似成立。无故障误差模型由状态方程y y Gx(1)给出,其中G为几何矩阵(n × p) (p = 3 +时钟状态数)y为测量集合(n × 1) εy为标称噪声(n × 1) x为位置和时钟未知数。标称噪声服从零均值高斯分布,协方差为1 W * *:1 0,y N W * * * *(2)故障误差模型故障误差模型是[7]中采用的模型,它概括了ram中使用的故障模式。在这个模型中,测量结果由一个误差模型决定,并且只有一个,在N +1个可能的误差模型中。这些误差模型或假设中的每一个都具有已知的发生概率pHi,并对应于在测量方程中添加未知状态:i i y y Gx ab <s:1>(3)a和b分别是一个n × mi矩阵和一个mi × 1向量。Ai是已知的,b是任意的。在本文的其余部分,我们将假设矩阵[gai]是满秩的,并且n>p+mi-1。如果干扰参数上没有变量的变化使矩阵[G Ai]满秩,则故障无法监测(例如,当A = G时)。同样,如果方程组(3)是待定的,当n<p+mi时将发生待定,则故障无法监测。无故障情况对应于i = 0。
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引用次数: 1
Capturing Method of Millimeter Displacement in Centimeter Class PPP-RTK Measured Data 厘米级PPP-RTK测量数据中的毫米位移捕获方法
Pub Date : 2019-04-11 DOI: 10.33012/2019.16812
Koki Asari, M. Saito, I. Mikami
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引用次数: 1
Analysis of Ionospheric Scintillation and its Impact on PPP at Low Latitudes 电离层闪烁分析及其对低纬度PPP的影响
Pub Date : 2019-04-11 DOI: 10.33012/2019.16842
K. Guo, M. Aquino, S. V. Veettil, Zhizhao Liu, Wu Chen, H. Marques
on developing novel GNSS receiver tracking models and scintillation mitigation tools, aiming to improve the receiver tracking performance under ionospheric scintillation. deployment of ionospheric scintillation and TEC monitoring receivers research focused on ionospheric effects on GNSS, including system vulnerability to ionospheric disturbances and relevant countermeasures. Nottingham Nottingham in European Commission, European Space Agency and UK research council funded projects. Her research focuses on assessing the effects of space weather on GNSS receivers and positioning errors aiming to improve the modeling of scintillation and to develop scintillation mitigation tools. are GNSS positioning system integrity, various GNSS applications, seamless positioning, and ABSTRACT Ionospheric scintillation refers to the random and rapid fluctuations in the amplitude and phase of radio signals that occur due to their propagation through plasma density irregularities in the ionosphere. For Global Navigation Satellite System (GNSS), scintillation can seriously degrade satellite signal quality and consequently the positioning accuracy, particularly at high and low latitude regions, where ionospheric disturbances are more frequent. This study analyzes the effects of scintillation on Global Positioning System (GPS) Precise Point Positioning (PPP), by making use of scintillation data recorded in Hong Kong during the solar maximum of 2014. Significant positioning error values of as much as 1.34 m in the up direction are observed with kinematic PPP processing under strong scintillation. The variations in the standard deviations of the carrier phase residuals in relation to satellite elevations and scintillation levels are investigated for the first time in this region. It is found that the standard deviation of carrier phase residuals increases depending on scintillation intensity. This study is important to help better understand the scintillation characteristics and its effects on GPS-based positioning in the Hong Kong region. It can also help in modelling the relationship between scintillation and carrier phase residuals, which can be of use in the development of scintillation mitigation approaches for PPP processing. scintillation on This also contribute to the modelling of ionospheric scintillation effects on phase residuals and to the development of scintillation mitigation tools for satellite-based positioning algorithms.
开发新的GNSS接收机跟踪模型和闪烁抑制工具,旨在提高接收机在电离层闪烁下的跟踪性能。电离层闪烁和TEC监测接收机的部署研究重点是电离层对GNSS的影响,包括系统对电离层干扰的脆弱性和相关对策。诺丁汉是由欧盟委员会、欧洲航天局和英国研究理事会资助的项目。她的研究重点是评估空间天气对GNSS接收机和定位误差的影响,旨在改进闪烁建模和开发闪烁缓解工具。电离层闪烁是指无线电信号在电离层中通过等离子体密度的不规则传播而产生的振幅和相位的随机和快速波动。对于全球卫星导航系统(GNSS)而言,闪烁会严重降低卫星信号质量,从而影响定位精度,特别是在电离层干扰较为频繁的高纬度和低纬度地区。本研究利用2014年太阳活动极大期在香港录得的闪烁数据,分析闪烁对全球定位系统(GPS)精确点定位(PPP)的影响。在强闪烁条件下,运动学PPP处理观测到向上定位误差高达1.34 m。在该地区首次研究了载波相位残差的标准差随卫星高度和闪烁水平的变化。发现载波相位残差的标准差随闪烁强度的增大而增大。本研究对了解香港地区的闪烁特征及其对gps定位的影响具有重要意义。它还有助于建立闪烁与载波相位残余之间关系的模型,这可用于开发用于PPP处理的闪烁缓解方法。这也有助于模拟电离层闪烁对相位残差的影响,并有助于开发用于卫星定位算法的闪烁减缓工具。
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引用次数: 2
Ionospheric Weather Observations with FORMOSAT-3/COSMIC and Prospects with FORMOSAT-7/COSMIC-2 FORMOSAT-3/COSMIC的电离层天气观测与FORMOSAT-7/COSMIC-2的展望
Pub Date : 2019-04-11 DOI: 10.33012/2019.16859
T. Liu, L. Chang, F. Chang, C. Chao
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引用次数: 1
Kalman Filter Derivation and Comparison to MUltiple SIgnal Classification (MUSIC) 卡尔曼滤波在多信号分类中的推导与比较
Pub Date : 2019-04-11 DOI: 10.33012/2019.16807
Russell Powell, Caleb Perry, A. Simmons, Gregory Reynolds, Clinton Blankenship
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引用次数: 0
期刊
Proceedings of the ION 2019 Pacific PNT Meeting
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