基于CORS系统的GPS接收机检测技术

介绍GPS接收机检定的主要指标,提出在无GPS标准基线检验场的情况下,结合利用连续运行参考站和GPS参考接收机对不同类型的接收机联合进行检测的方法,对建立用户自助检测接收机的测试评估技术体系进行探索性研究。     

内置ARM板卡GPS接收机设计与实现

随着信息化科技的不断发展,GPS在很多领域得到了广泛的应用。本文以GPS系统为蓝图,用ARM板卡技术作为平台设计了嵌入式GPS接收机,并对接收的动态试验数据精度进行分析,证明了基于ARM板卡的嵌入式GPS接收机在GPS系统中应用的可行性。     

GPS观测数据的仿真方法研究

在研究GPS系统的基础上建立GPS观测数据的仿真模型,编制相应的计算机程序,并根据该模型仿真了GPS的静态和地面低动态的观测数据,这对于论证GPS导航算法、设计GPS接收机等有一定的实用价值。     

多传感器与道路网数据用于汽车导航的研究

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。     

测量型GPS仪器比较

以科学的方法对Trimble、Topcon、南方测绘三个厂家GPS信号接收机和数据后处理软件进行比较。首先从GPS的发展历史和现状及其存在的问题进行分析研究,结合GPS系统和信号接收机的原理,对GPS结构等不同的方面进行分析比较,然后比较分析了各型号GPS的物理指标、精度指标、性能和价格,并对各型号GPS对应的数据后处理软件进行了实验分析,最后通过实验分析得出结论。     

Starfire 差分GPS服务介绍

对Starfire差分GPS服务系统的组成部分、各个部分的主要作用及相关的技术做了介绍 ,并对各种差分GPS方法的优缺点进行了比较 ,最后对Starfire差分GPS接收机的测试情况及定位结果进行了分析     

基于AR模型的GPS授时分析

由于GPS卫星采用高精度的星载原子钟,使得利用GPS接收机授时可以达到比较理想的精度。利用AR模型对GPS接收机的钟差数据进行建模分析,通过拟合比对,建立合适的预报模型,预报的精度达到了较好的效果。     

车载导航型GPS接收机的性能分析

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.     

GPS接收机检定原理及检定数据自动化处理思路探讨

通过对GPS接收机检定原理进行深入研究,参照《全球定位系统(GPS)测量型接收机检定规程》,推导GPS接收机各项检定内容的精度评定公式,对GPS接收机检定数据自动化处理进行探讨,并编写相应的精度分析软件以实现检定数据自动化处理功能。     

差分GPS水下立体定位导航系统的时间测量

差分GPS水下立体定位系统是通过测量同一水声信号到达不同浮标的时刻,计算水下收发机到各枚浮标的距离差,实现水下立体双曲线交会定位的。本文对水下立体定位导航系统的数学模型进行了推导。根据差分GPS水下立体定位导航系统的要求对GPS接收机时钟同步进行了详细分析,同时对GPS接收机接口数据输出和支持的三种时间测量方案进行了介绍,并对时间延迟进行了分析。     

Position and velocity reliability testing in degraded GPS signal environments

Reliability testing, namely receiver autonomous integrity monitoring (RAIM), consists of statistical testing of least-squares residuals of observations, e.g., on an epoch-by-epoch basis aiming towards reliable navigation fault detection and exclusion (FDE). In this paper, classic RAIM and FDE methods are extended with testing of range-rate residuals to find inconsistent velocity solutions in order to contribute to the reliability of the system with special focus on degraded signal environments. Reliability enhancement efforts discussed include a Backward-FDE scheme based on statistical outlier detection and an iteratively reweighted robust estimation technique, a modified Danish method. In addition, measurement weighting assigned to code and Doppler observations is assessed in the paper in order to allow fitting a priori variance models to the estimation processes. The schemes discussed are also suitable in terms of computational convenience for a combined GPS/Galileo system. The objective of this paper is to assess position and velocity reliability testing and enhancement in urban and indoor conditions and to analyze the navigation accuracy conditions with high sensitivity GPS (HSGPS) tests. The results show the necessity of weighted estimation and FDE for reliability enhancement in degraded signal-environment navigation.     

建立GPS控制网观测方案优化的研究

利用GPS定位技术建立各种用途控制网已经相当普及.针对GPS控制网建立前观测方案的优化设计进行研究,探讨接收机的适用条件以及GPS观测时间的确定.实验数据证明接收机的选择和观测时间的确定对控制网控制质量是很重要的,实验分析结果既可为GPS科研工作的深入研究提供参考,亦可为从事高精度GPS测量生产应用提供借鉴.     

Automated GPS processing for global total electron content data

A software package known as MIT Automated Processing of GPS (MAPGPS) has been developed to automate the processing of GPS data into global total electron density (TEC) maps. The goal of the MAPGPS software is to produce reliable TEC data automatically, although not yet in real time. Observations are used from all available GPS receivers during all geomagnetic conditions where data has been successfully collected. In this paper, the architecture of the MAPGPS software is described. Particular attention is given to the algorithms used to estimate the individual receiver biases. One of the largest sources of error in estimating TEC from GPS data is the determination of these unknown receiver biases. The MAPGPS approach to solving the receiver bias problem uses three different methods: minimum scalloping, least squares, and zero-TEC. These methods are described in detail, along with their relative performance characteristics. A brief comparison of the JPL and MAPGPS receiver biases is presented, and a possible remaining error source in the receiver bias estimation is discussed. Finally, the Madrigal database, which allows Web access to the MAPGPS TEC data and maps, is described.     

Performance of GPS and GPS/SINS navigation in the CE-5T1 skip re-entry mission

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.     

GPS接收机内噪声水平的评价与检测方法

论文结合某品牌GPS接收机检测实例,提出了GPS接收机内噪声水平分布统计的评价方法,以及在超短基线场内GPS接收机内噪声水平的全新检测方法———多时段旋转检测台法。实例测试,按本方法得到的被测试GPS接收机内噪声水平标准差为0.38mm。由测试实例得到如下结论:本文的GPS接收机内噪声水平评价方法以及检测方法更加合理、可信;在超短基线场内多时段测得的同一基线长度互差应小于2mm;GPS接收机系统软件的抗噪性能对内噪声水平有着非常重要的影响。     

GPS接收机硬件延迟时变特性分析

在全球定位系统(Global Positioning System，GPS)中，接收机硬件延迟引起的码偏差和相位偏差是影响精密授时、电离层建模以及非差模糊度解算的重要因素。利用GPS对电离层总电子含量进行估计和建模时，通常假定GPS接收机硬件延迟偏差是稳定不变的量，对其可能存在的波动及影响因素考虑不充分。因此，对GPS接收机硬件延迟偏差的时变特性进行分析，有助于提高电离层电子含量估值的准确性和可靠性。分析了GPS接收机差分码偏差(differential code bias，DCB)和差分相位偏差(differential phase bias，DPB)单历元及单天解的时间变化特性，并对温度变化与接收机DCB、DPB变化之间的相关性进行了实验探究。结果表明，接收机重启前后其DCB值会发生突变，重启之后接收机DCB和DPB大约需要25 min才能趋于稳定。接收机DCB和DPB并不能长期保持稳定，实验数据显示，在2~3 h内，DCB的变化量可以达到0.8 m左右，DPB的变化量可以达到4 mm左右，接收机DCB和DPB的波动与周围环境温度的变化具有较强相关性。     

Design of a low-cost attitude determination GPS/INS integrated navigation system

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.     

GBAS testbed development in Taiwan with a prototype GPS/GBAS receiver

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.