共查询到19条相似文献，搜索用时 78 毫秒
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针对能够标识北斗二号与北斗三号系统服务完好性的参数差异问题,该文从完好性参数定义、导航电文结构、参数内容和播发方式等方面对北斗二号和北斗三号系统完好性参数播发现状进行了比对分析,并对各类参数的工程实现情况进行了比较,结果表明:在兼容北斗二号基本导航服务相关系统完好性参数的基础上,北斗三号增加了可快速标识服务精度及预测精度的完好性参数;受多方面的约束与局限,北斗二号仅具备提供单频改正的广域差分增强服务的能力,且无相关国际标准规范支撑,而北斗三号为能获取国际民航组织测试认证,已立足于国际相关标准规范进行了可支撑单、双频改正的星基增强服务工程实现. 相似文献
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为了提高GPS卫星导航系统服务性能,很多国家和地区建立了独立的星基增强系统(SBAS),通过提供广播星历差分与完好性增强信息,满足高精度高完好性用户使用需求。本文介绍了美国WAAS和欧洲EGNOS等星基增强系统的广播星历差分完好性信息电文编码格式,并对实际星基增强系统的广播星历差分与完好性电文进行解析。由于不同的星基增强系统采用的信息处理模式不同,针对WAAS和EGNOS两个不同地区建立的星基增强系统,对广播星历差分慢变改正／快变改正的变化特征进行了比较分析。研究了星基增强系统广播星历差分完好性信息用户使用算法,基于国际GNSS服务组织(IGS)提供的GPS实测数据,对WAAS系统和EGNOS系统的广播星历差分服务精度和完好性性能进行了对比分析。结果表明,WAAS系统的伪距单点定位精度约为1.2 m, EGNOS系统的伪距单点定位精度约为1.8 m,与GPS基本导航服务相比,伪距单点定位精度可提高约22％和16％。两个星基增强系统利用完好性电文计算的完好性保护限值大致相当,均在16 m以内,能够对定位误差进行包络。 相似文献
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本文地伪距观测值的误差分布,推导几种在空间导航增强系统中应用的完好性方程,并得出完好性方程与误差分布有密切关系的结论。 相似文献
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针对导航卫星在区域完好性监测网可视弧段之外难以实现基于地面监测站的系统级完好性监测问题,提出一种基于星间链路辅助支持的导航卫星自主完好性监测方法。该方法通过利用星间组合观测值,分离星钟误差和星历误差,采用基于平稳时间序列的非稳态异常检测算法对导航卫星星载原子钟相位抖动及频率的异常漂移进行监测;采用基于轨道先验信息的非中心化开方分布异常检测算法对轨道异常机动进行监测,并利用星间链路组合观测量对卫星自主完好性监测及其对全球用户完好性性能的提升作用开展仿真分析与研究。仿真计算结果表明:该方法可以在地面监测网不可视弧度内有效减小空间段卫星部分的故障漏检概率以及系统完好性风险,缩短完好性告警时间,提高全球卫星导航系统的完好性服务水平。 相似文献
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导航系统的完好性是指系统在不能使用时,及时向用户发出告警的能力。北斗卫星导航系统完好性研究处于刚起步阶段,实施办法、实验监测和衡量标准急需建立和完善。本文对北斗卫星导航系统完好性性能测试方法进行了深入研究,提出了适用于北斗二代导航系统完好性性能的监测方法。 相似文献
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针对生命安全用户对导航系统高完好性服务能力的迫切需求,以及国际航空完好性服务竞争日趋激烈的现状,北斗全球卫星导航系统一体化设计和规划了北斗星基增强系统(BDSBAS)。该文从国际民航组织(ICAO)相关标准要求,对BDSBAS服务性能进行研究和分析,推导并论证了系统精度、完好性、连续性等主要指标的分解方法;在此基础上,仿真计算了BDSBAS不同航空完好性服务等级对北斗系统等效伪距测量误差(UERE)、卫星故障概率、虚警概率等方面性能的要求。相关研究与分析结果能够为北斗及BDSBAS工程建设提供有益参考和借鉴。 相似文献
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基于漏检概率的RAIM可用性分析方法 总被引：9，自引：2，他引：9
描述了通常基于单故障假设相应的HPL，或VPL，的计算模型，针对WAAS用户在应用RAIM时需要顾及多故障的情况，提出了基于漏检概率的可用性分析方法，并通过模拟计算得到一些结论。 相似文献
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利用GALILEO全球监测网络和中国地壳运动监测网络分别对GALILEO系统完备性指标SISMA进行仿真计算。结果表明,全球完备性监测SISMA结果不稳定,随地理位置的变化较大,不能满足局部地区的生命安全服务要求;利用适当布设的局域监测网络进行的SISMA局域监测数值稳定,变化较小,结果明显优于全球SISMA监测结果,可以满足生命安全服务要求,可信度达到100%。在我国进行局域SISMA监测,是对全球完备性监测进行的有效和必要补充,提高系统的可用性和定位可信度。 相似文献
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WAAS系统下单频GPS用户电离层延迟改正新方法 总被引：5，自引：2，他引：3
对于现有WAAS等差分GPS系统而言,在电离层活动激烈及系统不能正常发送或用户无法正常接收电离层延迟改正信息时,如何确保其所服务区域内单频GPS用户的电离层延迟的实时改正效果,是需要进一步解决的问题。本文提出一种能够同时克服这些不足的单频GPS电离层延迟实时改正方案,并用算例初步验证了其有效性。 相似文献
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The Federal Aviation Administration (FAA) is developing the wide-area augmentation system (WAAS) to supplement the Global
Positioning System (GPS) and serve as a single en-route navigation aid. The program traveled a rocky road so far. We compare
the original concept of WAAS with its current scaled down version, analyze the changed perspectives with respect to the utility
of GPS for air navigation and the concomitant role of WAAS, and explore the future of GPS/WAAS. ? 2000 John Wiley & Sons,
Inc. 相似文献
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The ionospheric impact of the October 2003 storm event on Wide Area Augmentation System 总被引：4，自引：2，他引：2
The United States Federal Aviation Administrations (FAA) Wide-Area Augmentation System (WAAS) for civil aircraft navigation is focused primarily on the Conterminous United States (CONUS). Other Satellite-Based Augmentation Systems (SBAS) include the European Geostationary Navigation Overlay Service (EGNOS) and the Japanese Multi-transport Satellite-based Augmentation System (MSAS). Navigation using WAAS requires accurate calibration of ionospheric delays. To provide delay corrections for single frequency global positioning system (GPS) users, the wide-area differential GPS systems depend upon accurate determination of ionospheric total electron content (TEC) along radio links. Dual-frequency transmissions from GPS satellites have been used for many years to measure and map ionospheric TEC on regional and global scales. The October 2003 solar-terrestrial events are significant not only for their dramatic scale, but also for their unique phasing of solar irradiance and geomagnetic events. During 28 October, the solar X-ray and EUV irradiances were exceptionally high while the geomagnetic activity was relatively normal. Conversely, 29–31 October was geomagnetically active while solar irradiances were relatively low. These events had the most severe impact in recent history on the CONUS region and therefore had a significant effect on the WAAS performance. To help better understand the event and its impact on WAAS, we examine in detail the WAAS reference site (WRS) data consisting of triple redundant dual-frequency GPS receivers at 25 different locations within the US. To provide ground-truth, we take advantage of the three co-located GPS receivers at each WAAS reference site. To generate ground-truth and calibrate GPS receiver and transmitter inter-frequency biases, we process the GPS data using the Global Ionospheric Mapping (GIM) software developed at the Jet Propulsion Laboratory. This software allows us to compute calibrated high resolution observations of TEC. We found ionospheric range delays up to 35 m for the day-time CONUS during quiet conditions and up to 100 m during storm time conditions. For a quiet day, we obtained WAAS planar fit slant residuals less than 2 m (0.4 m root mean square (RMS)) and less than 25 m (3.4 m RMS) for the storm day. We also investigated ionospheric gradients, averaged over distances of a few hundred kilometers. The gradients were no larger than 0.5 m over 100 km for a quiet day. For the storm day, we found gradients at the 4 m level over 100 km. Similar level gradients are typically observed in the low-latitude region for quiet or storm conditions. 相似文献
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地基完好性监测是利用四个或四个以上的精确坐标的监测站对卫星进行监测,计算其星历及星钟误差。该方法需满足四重以上监测站覆盖条件,对于自主导航和区域布站的导航系统不能实现导航卫星的全弧段完好性监测。对于不满足上述覆盖条件的卫星,采用基于星间链路的监测方法,利用四个或四个以上的具有一定坐标误差的卫星对该卫星进行监测。通过星历数据和星间测距数据计算SISMA,从而进行导航卫星全弧段的完好性监测。 相似文献
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For the commonly used GPS wide-area augmentation systems (WAAS) with a grid ionospheric model, the efficient modelling of
ionospheric delays in real time, for single-frequency GPS users, is still a crucial issue which needs further research. This
is particularly necessary when differential ionospheric delay corrections cannot be broadcast, when users cannot receive them,
or when there are ionospheric anomalies. Ionospheric delays have a severe effect on navigation performance of single-frequency
receivers. A new scheme is proposed which can efficiently address the above problems. The robust recurrence technique is based
on the efficient combination of single-frequency GPS observations by users and the high-precision differential ionospheric
delay corrections from WAAS. Its effectiveness is verified with examples.
Received: 24 December 1999 / Accepted 21 February 2001 相似文献