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GPS观测数据文件及其解码 总被引：1，自引：0，他引：1
本文在系统分析了GPS观测数据文件的结构和文件中数据的表示方法之后，详细论述了二进制文件转换方法、数据完整性和有效件检验的内容及解码输出文件的格式。最后，提出了作者在编写了多种接收机数据解码程序后得出的几点结论和设想。 相似文献
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在全球卫星导航系统的研究和测量工作中,需要对GNSS测量数据进行分析和计算,解码GPS接收机原始数据是实时获得以上数据的主要方法。原始电文的二进制格式由各接收机板卡厂商及板卡集成厂家定义本文介绍了常用原始GNSS数据格式内容并对其进行解码转化为标准的RINEX格式文件。该解码软件可以对多种数据格式的电文进行分析解码得到相应的多系统观测文件和星历文件,包括BDS三频数据,并可以根据需要选择生成的RINEX文件中系统类型。使用TEQC软件对数据质量进行进一步的质量分析,为后续的数据分析和处理提供了可靠的保障。 相似文献
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首先介绍了能进行静态与实时动态数据采集的GNSS天线阵列接收机(最多可连接8个天线)的研制过程,该接收机通过GNSS OEM板与天线阵列共享设备的集成,大大降低了监测成本。基于研制的GNSS天线阵列接收机,详细讨论了观测数据的解码方法。采用美国天宝公司的BD970 OEM模块,在详细分析二进制消息格式的基础上,研制了数据采集与解码软件,并通过实际应用,证明了该系统可用于大坝、滑坡等的变形监测中,具有广泛的应用前景。 相似文献
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范福平 《测绘与空间地理信息》2021,44(6):141-144
在进行伪距单点定位时,数据往往采用后处理的方式,传统的精密卫星轨道及钟差产品存在时间延迟的问题,限制了单点定位技术在实时场景的应用.利用数据质量实时分析和评价的方法,开发高精度的GNSS实时数据解码技术,并对定位服务进行性能测试,得到实时伪距单点定位结果.通过实验发现,定位精度达到厘米级.实时解码系统具有可操作性与可行性.加入实时轨道和钟差的改正,伪距单点定位的精度也随之提升.本文通过对实时观测数据流解码,将伪距单点定位和实时观测数据解码模块融合,实现了实时伪距单点定位. 相似文献
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In this paper, we present the development of a local area differential GPS testbed of the ground-based augmentation system (GBAS) as the future airport navigation facility in the Taipei Flight Information Region (FIR) in Taiwan. The testbed is mainly a GBAS ground facility, which consists of a ground station, three GBAS receivers, and a VDL (VHF data link) broadcast antenna. We also present an airborne GPS/GBAS prototype receiver in this paper. The airborne subsystem (a GPS/GBAS receiver) receives the correction messages from the ground subsystem to perform a differential GPS (DGPS) positioning. In order to provide an ILS-look-alike approach and landing, the output messages of the airborne receiver are packed in an ARINC 429 format. The proposed airborne system has a software-based global navigation satellite system (GNSS) receiver structure. 相似文献
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为了系统验证SINS／GPS紧组合系统的性能,基于GPS软件接收机,进行了仿真系统构建。仿真系统由轨迹发生器、GPS中频信号模拟器、IMU信号模拟器、GPS软件接收机、SINS导航解算模块、组合滤波算法和导航性能分析模块等部分构成,其中详细设计了GPS软件接收机中的捕获和跟踪算法、SINS解算以及基于伪距和伪距率的组合滤波算法。仿真结果表明：紧组合导航系统收敛性较好,能够一定程度上抑制惯导系统误差的积累,有较好的导航性能。设计的该系统满足紧组合导航系统性能验证的需要,也为后续的超紧组合研究奠定了良好的基础。 相似文献
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结合一般GPS接收机性能分析要求,针对导航型GPS接收机主要用于车栽动态导航定位的特点,提出了主要包括一般性能检验、导航精度测试、不同环境下的导航性能测试等较为全面的车载导航接收机的性能综合分析方法.基于此方法对一款导航型接收机进行了综合性能测试,得出了有益的结论. 相似文献
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Dong-Hwan Hwang Sang Heon Oh Sang Jeong Lee Chansik Park Chris Rizos 《GPS Solutions》2005,9(4):294-311
Due to their complementary features of GPS and INS, the GPS/INS integrated navigation system is increasingly being used for
a variety of commercial and military applications. An attitude determination GPS (ADGPS) receiver, with multiple antennas,
can be more effectively integrated with a low-cost IMU since the receiver gives not only position and velocity data but also
attitude data. This paper proposes a low-cost attitude determination GPS/INS integrated navigation system. The proposed navigation
system comprises an ADGPS receiver, a navigation computer unit (NCU), and a low-cost commercial MEMS IMU. The navigation software
includes a fault detection and isolation (FDI) algorithm for integrity. In order to evaluate the performance of the proposed
navigation system, two flight tests have been performed using a small aircraft. The first flight test confirmed the fundamental
operation of the proposed navigation system and the effectiveness of the FDI algorithm. The second flight test evaluated the
performance of the proposed navigation system and demonstrated the benefit of GPS attitude information in a high dynamic environment.
The flight test results show that the proposed ADGPS/INS integrated navigation unit gives reliable navigation performance
even when anomalous GPS data is provided and gives better navigation performance than a conventional GPS/INS unit. 相似文献
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A CE-5T1 spacecraft completed a high-speed skip re-entry to the earth after a circumlunar flight on October 31, 2014. In addition to the strapdown inertial navigation system (SINS), a lightweight GPS receiver with rapid acquisition was developed as a navigation sensor in the re-entry capsule. The GPS receiver effectively solved the poor accuracy problem of long-term navigation using only the SINS. In contrast to ground users and low-earth-orbit spacecraft, numerous factors, including high altitude and kinetic characteristics in high-speed skip re-entry, are important for GPS positioning feasibility and were presented in accordance with the flight data. GPS solutions started at nearly 4900 km orbital altitude during the phases of re-entry process. These solutions were combined by an inertial measurement unit in a loosely coupled integrated navigation method and SINS navigation initialization. A simplified GPS/SINS navigation filter for limited resources was effectively developed and implemented on board for spacecraft application. Flight data estimation analyses, including trajectory, attitude, position distribution of GPS satellite, and navigation accuracy, were presented. The estimated accuracy of position was better than 42 m, and the accuracy of velocity was better than 0.1 m/s. 相似文献
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针对在导航实践中低成本MEMS使用传统紧耦合方法计算精度受到限制的问题,提出了一种采用载波相位平滑伪距GNSS PPP/INS紧耦合的算法。实验表明,使用相位平滑伪距的GNSS PPP/INS紧耦合方法后低精度的MEMS和GPS组合位置精度为dm级,速度精度为cm/s甚至mm/s,比传统C/A码紧耦合定位精度高,有较好的收敛性;其次当增加相位平滑的历元数后精度也相应提高。当出现GPS信号中断时,该方法能够加速中断以后滤波收敛的速度,将导航精度控制在中高精度惯导作业要求范围内。该方法节约了导航作业的设备成本,具有一定实际意义。 相似文献
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多传感器与道路网数据用于汽车导航的研究 总被引：4，自引：0，他引：4
对车载导航系统中GPS接收机，车论计数器和电子罗盘传感器数据与导航电子地图所提供的道路网络数据进行了综合处理，建立了道路网络数据的网络拓扑关系，在此基础上提出了基于道路网络拓扑关系，利用GPS接收机，车轮计数器和电子罗盘传感器对汽车进行实时定位的算法。最后，对导航中汽车的定位误差进行了分析。实验证明，GPS接收机，车轮计数器和电子罗盘传感器与道路网络数据综合，在导航过程中能够补偿GPS信号技失，实时、高精度、高可靠性地确定汽车的位置。 相似文献