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Proceedings of the ION 2019 Pacific PNT Meeting最新文献

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Integration of GNSS-PPP and IMU/SPEED Sensors in Urban Areas 城市地区GNSS-PPP和IMU/SPEED传感器的集成
Pub Date : 2019-05-01 DOI: 10.33012/2019.16782
N. Kubo, Yize Zhang, Daisuke Hatta
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引用次数: 4
Hyper-parameter Comparison on Convolutional Neural Network for Visual Aerial Localization 卷积神经网络视觉航空定位的超参数比较
Pub Date : 2019-05-01 DOI: 10.33012/2019.16846
J. M. Berhold, R. Leishman, B. Borghetti, D. Venable
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引用次数: 0
SIS Monitoring for ARAIM in the Absence of Precise Clock Estimates 在没有精确时钟估计的情况下对ARAIM进行SIS监测
Pub Date : 2019-05-01 DOI: 10.33012/2019.16838
Kazuma Gunning, T. Walter, David Powell
This paper describes methods for constellation monitoring in the absence of external precise clock estimates. Careful characterization of constellation performance is necessary for the use of Advanced RAIM (ARAIM). In particular, the narrow (Psat) and wide (Pconst) fault rates must be determined. However, typical constellation monitoring approaches rely on the comparison between the broadcast ephemeris and precise estimates of the satellite orbit and clock, and these may not always be available. Furthermore, they may only monitor reference signals that will not actually be operationally used. This paper describes a method to independently estimate satellite clock and differential code biases in order to evaluate the ranging performance of GPS and GLONASS for ARAIM. Daily variations in the L1 C/A-L5Q clock and differential code bias are examined and quantified. Finally, GLONASS faults are closely examined using the clock estimation techniques.
本文介绍了在没有外部精确时钟估计的情况下星座监测的方法。对星座性能进行仔细的表征对于使用先进防空导弹(ARAIM)是必要的。特别是,必须确定窄(Psat)和宽(Pconst)故障率。然而,典型的星座监测方法依赖于广播星历与卫星轨道和时钟的精确估计之间的比较,而这些可能并不总是可用的。此外,它们可能只监视实际上不会在操作中使用的参考信号。本文介绍了一种独立估计卫星时钟和差分码偏差的方法,以评估GPS和GLONASS的ARAIM测距性能。L1 C/A-L5Q时钟和差分码偏差的日常变化进行了检查和量化。最后,使用时钟估计技术仔细检查GLONASS故障。
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引用次数: 2
Seasonality of the Local-time Variations in Formosat-3/COSMIC S4 Indices and Ionospheric Electron Density Formosat-3/COSMIC S4指数和电离层电子密度局地变化的季节性
Pub Date : 2019-05-01 DOI: 10.33012/2019.16803
C. S. Salinas, L. Chang
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引用次数: 0
A Novel Application of Deformation Monitoring using GNSS-R Technology 基于GNSS-R技术的变形监测新应用
Pub Date : 2019-05-01 DOI: 10.33012/2019.16831
Yang Yang, Yu Zheng, Wenkun Yu, D. Weng, Wenbin Li, Wu Chen
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引用次数: 1
The FengYun-3 Radio Occultation Sounder GNOS: A Review of the Missions and Early Results 风云三号无线电掩星探测仪GNOS:任务回顾与早期成果
Pub Date : 2019-05-01 DOI: 10.33012/2019.16833
Yueqiang Sun, Congliang Liu, W. Bai, Yan Liu, Q. Du, Xianyi Wang, Guanglin Yang, M. Liao, Zhongdong Yang, Xiaoxin Zhang, X. Meng, Danyang Zhao, Junming Xia, Yuerong Cai, G. Kirchengast
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引用次数: 1
Distance Determination Between WGS84 Coordinates: An Assessment of Approximation Methods for Reduced Computational Complexity WGS84坐标之间的距离确定:一种降低计算复杂度的近似方法的评估
Pub Date : 2019-04-11 DOI: 10.33012/2019.16809
David Seiferth, C. Blum, M. Heller, F. Holzapfel
Due to the enormous fields of application, Unmanned Air Systems (UAS) nowadays differ inter alia in size, weight, thrust and range. The high diversity of application imposes a broad range of requirements to the flight control software of the Unmanned Air Vehicle in terms of complexity, computational effort and tracking performance. Trajectory flights based on way-points, automatic take-off and landing capabilities, or safe area detection and adherence algorithms require reliable and accurate distance and flight path calculation methodologies. This paper reviews, analyses and evaluates seven different methods to calculate the shortest distance and its corresponding flight path course between coordinates on the WGS84 reference ellipsoid. Depending on the operating distance of the UAS, the accuracy and the computational complexity can be reduced dramatically by utilizing an application-adapted calculation method. This paper recommends the suitable approximation method for the application of your Unmanned Air Vehicle System. Since the computational complexity gets rising significance due to software verification and safety assessment the distance calculation should be kept as simple as feasible by utilizing the appropriate distance calculation method while maintaining accuracy and tracking performance. The feasibility of the proposed methods is discussed for three different typical application scenarios.
由于应用领域巨大,无人机系统(UAS)如今在尺寸,重量,推力和范围等方面有所不同。应用的高度多样性对无人机飞行控制软件的复杂性、计算量和跟踪性能提出了广泛的要求。基于航路点、自动起降能力或安全区域检测和粘附算法的轨迹飞行需要可靠和准确的距离和飞行路径计算方法。本文对WGS84参考椭球上坐标之间的最短距离及其对应的航路航线的七种不同计算方法进行了综述、分析和评价。根据无人机操作距离的不同,采用适合实际应用的计算方法可以大大降低精度和计算复杂度。本文推荐了适合于无人机系统应用的近似方法。由于软件验证和安全评估导致的计算复杂度越来越大,因此在保持精度和跟踪性能的同时,应采用适当的距离计算方法,使距离计算尽可能简单。针对三种不同的典型应用场景,讨论了所提出方法的可行性。
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引用次数: 3
Model-based Threshold and Centerline Detection for Aircraft Positioning during Landing Approach 基于模型的飞机进场定位阈值和中心线检测
Pub Date : 2019-04-11 DOI: 10.33012/2019.16787
S. Wolkow, Maik Angermann, Andreas Dekiert, U. Bestmann
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引用次数: 4
Application Research of IGS Products in GPS Real-time Positioning and Timing IGS产品在GPS实时定位授时中的应用研究
Pub Date : 2019-04-11 DOI: 10.33012/2019.16854
Ran Yan, Jian-Feng Wu, Yonghui Hu
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引用次数: 0
Instantaneous Decimeter-level Positioning using Triple-frequency GPS/BeiDou/Galileo/QZSS Data Over Wide Areas 基于三频GPS/北斗/伽利略/QZSS数据的广域瞬时分米级定位
Pub Date : 2019-04-11 DOI: 10.33012/2019.16786
J. Geng, Jiang Guo, Hua Chang, Ran Zeng
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引用次数: 0
期刊
Proceedings of the ION 2019 Pacific PNT Meeting
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