共查询到20条相似文献，搜索用时 15 毫秒
1.
欧盟在2010-04-13首次正式发布了Galileo公开服务空间信号接口控制文档(Galileo OS SIS ICD),标志着Galileo系统建设从概念设计、在轨验证到系统实施又迈进了重要一步,对全球导航卫星系统(GNSS)的发展具有重要意义。通过与GPS接口说明文档比较,解析了Galileo OS SIS ICD中导航电文结构设计和内容设计方面的思路和特点。解析表明,与GPS L1 C/A码导航电文设计相比,Galileo OS在导航电文设计上既有继承、亦有创新。整体设计体现了开放和灵活的特点,特别是在电文页流结构、电文星间交叉播发、兼容和互操作以及完好性方面的设计既体现了GNSS技术的发展,又体现了GNSS设计理念的进步。Galileo导航电文的设计理念不仅可为我国北斗卫星导航系统电文的设计提供参考,而且有利于加强与Galileo系统之间的互操作研究。 相似文献
2.
We present experimental results showing the impact of the proposed LightSquared (LS) Long-term Evolution (LTE) signals on both GPS and Galileo civil modulations in the L1/E1 band. The experiments were conducted in radiated mode in a large anechoic chamber. Three Galileo enabled receivers were chosen for the tests, and a state of the art GNSS signal generator was used to simulate both GPS and Galileo signals. The LTE signals were generated by an Agilent Programmable Signal Generator with a license to generate the signals according to the 3GPP LTE FDD standard. The interference impact was measured in terms of a Carrier-to-Noise power spectral density ratio (C/N 0) degradation, in accordance with the methodology which the LS/GPS Technical Working Group (TWG) established by mandate of the FCC. A model for determining the impact of the LS signal on the considered GNSS signals is provided and is validated against experimental data. It is shown that the Galileo E1 Open Service (OS) signal is marginally more susceptible to this form of interference than the GPS L1 C/A signal due to its greater proximity to the lower edge of the L1 band. The impact of LS interference was further analyzed in terms of pseudorange and position errors. Despite its relevance for most GNSS users, this aspect was not considered by the TWG. Measurement and position domain analysis along with the study of the LS impact on the Galileo OS signals are the major contributions. The analysis confirms the results obtained by the TWG and shows that the receiver front-end plays a major role in protecting GNSS signals against RF interference. While it appears that, for now, the LS network will not be deployed, the approach taken and the results obtained herein can be readily adapted for any future terrestrial mobile network that may take the place of LS. 相似文献
3.
Sergey S. Pospelov Andrey L. Botchkovski Peter A. Krauss Stefan Berberich 《GPS Solutions》2000,4(1):48-55
Software Global Navigation Satellite Systems (GNSS) receivers are those that implement signal correlation processing not in
hardware, but in their software. The main problem for the development of real-time software (SW) multichannel GNSS receivers
is the tremendous amount of calculations to perform signal correlation.
The article reviews recent developments of SW GNSS receivers. The emphasis is made on the computationally effective correlation
processing algorithms and the optimization of processing allocation to the receiver's hardware (HW) and SW.
An architecture is suggested that implements the PRN signals despreading in a special HW preprocessor while all the other
correlation processing functions are still kept in SW. The combination of the most time-consuming processing in HW, and all
signal structure-dependent processing in SW, enables unique flexibility of sophisticated GNSS receiver design based on inexpensive
digital signal processors. ? 2000 John Wiley & Sons, Inc. 相似文献
4.
The growth of innovative positioning-related services and applications within the wireless mass-market, and the green light
for the development and modernization of Global Navigation Satellite Systems (GNSS) catalyze the research activity in the
navigation field both at the system and user levels. In addition, different government institutions are working toward the
definition of navigation plans and regulations which will require accurate locations of mobile users in case of emergency (US E-911 law and the European
E-112 directive). From the technical standpoint, within every navigation/positioning system which will be available in the
near future, the user terminal will play a central role. In fact, if navigation signals from different sources are available,
the unique possibility to obtain the best navigation performance from the user perspective will be the employment of enhanced
smart receivers able to fuse different data. With this aim, the Software Defined Radio (SDR) technology can be successfully employed for the design of innovative navigation receivers. The main goal of this paper is
to present the overall SDR receiver architecture, focusing attention on reconfigurability and flexibility issues which are
guaranteed by the use of reprogrammable high-speed hardware (FPGA–Field Programmable Gate Array and DSP–Digital Signal Processor).
The direct benefit of such an implementation is the possibility to obtain a deep integration at the raw signal level between
GPS and the future Galileo; the interoperability issue among different systems is then solved at the receiver level.
Electronic Publication 相似文献
5.
全球导航卫星系统（Global Navigation Satellite System,GNSS）探测大气电离层需要精确处理由接收机差分码偏差（differential cade bias,DCB）引起的系统误差。准确掌握接收机DCB的多时间尺度精细变化等特性是联合美国GPS、中国北斗卫星导航系统（BeiDou navigation satellite system,BDS）和欧盟Galileo等多GNSS技术监测电离层所面临的主要科学问题之一。为此,提出了基于零基线精密估计站间单差接收机DCB的方法,并对站间单差接收机DCB的日加权平均值进行了分析。基于4台多模接收机采集于2013年的双频观测值,揭示了站间单差接收机DCB的变化可能受3种因素的影响,即接收机内置软件的版本升级（实验中引起了约3 ns的显著增加）、拆卸个别接收机所导致的观测条件改变（实验中引起了约1.3 ns的显著减少）和估计方法的误差（引起了与导航系统卫星几何结构重复性相一致的周期性变化）等。 相似文献
6.
目前,全球卫星导航系统(GNSS)已进入以GPS、GLONASS、BDS、Galileo四系统为代表的多系统并存的时代,多系统多频率观测值的综合应用极大地提升了GNSS的服务能力. GNSS自身的数据质量是取得高精度结果的先决条件之一,也是多系统精密定位随机模型构建的关键. 为避免码分多址和频分多址机制不同的影响,本文采用几何无关和M-W组合方法,基于科廷大学实测零基线数据对四系统的载波相位单差残差序列对比分析,并利用高度角随机模型中的正弦模型和指数模型对载波相位观测值精度随高度角变化建模,获得适用于不同系统不同频率观测值的随机模型. 实验分析表明,单差残差序列随高度角变化情况在不同系统不同频率表现出不同特性;Galileo系统L1、L2观测值精度相当,均在0.9 mm左右,其他系统则表现出L2精度比L1精度更差的性质. 高度角加权模型拟合结果表明,正弦模型和指数模型对GPS和Galileo系统的L1、L2精度序列拟合一致性较好,而BDS系统使用正弦模型拟合效果略差,GLONASS系统则不适合采用正弦模型评估L2观测值精度. 相似文献
7.
In this work, a regional network of permanent Global Navigation Satellite Systems (GNSS) receivers is used to estimate the decorrelation of the spatially correlated errors in differential GNSS positioning. Emphasis is laid on the dispersive errors (i.e. mainly the ionosphere). A new index, based on variance as function of station separation (semivariance) is proposed and compared to the existing I95 index. This study uses data from the 29–30th October 2003, a period with severe ionospheric activity. The proposed index is shown to give realistic predictions of differential measurement accuracy, and has potential for further development towards use in RTK-networks. 相似文献
8.
Successful carrier phase ambiguity resolution is the key to high-precision positioning with Global Navigation Satellite Systems
(GNSS). The ambiguity dilution of precision (ADOP) is a well-known scalar measure which can be used to infer the strength
of the GNSS model for carrier phase ambiguity resolution. In this contribution we present analytical closed-form expressions
for the ADOP. This will be done for a whole class of different multi- frequency single baseline models. These models include
the geometry-fixed, the geometry-free and the geometry-based models, respectively. And within the class of geometry-based
models, we discriminate between short and long observation time spans, and between stationary and moving receivers. The easy-to-use
ADOP expressions can be applied to infer the contribution of various GNSS model factors. They comprise, for instance, the
type, the number and the precision of the GNSS observations, the number and selection of frequencies, the presence of atmospheric
disturbances, the length of the observation time span and the length of the baseline. 相似文献
9.
Krzysztof Sośnica Lars Prange Kamil Kaźmierski Grzegorz Bury Mateusz Drożdżewski Radosław Zajdel Tomasz Hadas 《Journal of Geodesy》2018,92(2):131-148
The space segment of the European Global Navigation Satellite System (GNSS) Galileo consists of In-Orbit Validation (IOV) and Full Operational Capability (FOC) spacecraft. The first pair of FOC satellites was launched into an incorrect, highly eccentric orbital plane with a lower than nominal inclination angle. All Galileo satellites are equipped with satellite laser ranging (SLR) retroreflectors which allow, for example, for the assessment of the orbit quality or for the SLR–GNSS co-location in space. The number of SLR observations to Galileo satellites has been continuously increasing thanks to a series of intensive campaigns devoted to SLR tracking of GNSS satellites initiated by the International Laser Ranging Service. This paper assesses systematic effects and quality of Galileo orbits using SLR data with a main focus on Galileo satellites launched into incorrect orbits. We compare the SLR observations with respect to microwave-based Galileo orbits generated by the Center for Orbit Determination in Europe (CODE) in the framework of the International GNSS Service Multi-GNSS Experiment for the period 2014.0–2016.5. We analyze the SLR signature effect, which is characterized by the dependency of SLR residuals with respect to various incidence angles of laser beams for stations equipped with single-photon and multi-photon detectors. Surprisingly, the CODE orbit quality of satellites in the incorrect orbital planes is not worse than that of nominal FOC and IOV orbits. The RMS of SLR residuals is even lower by 5.0 and 1.5 mm for satellites in the incorrect orbital planes than for FOC and IOV satellites, respectively. The mean SLR offsets equal \(-44.9, -35.0\), and \(-22.4\) mm for IOV, FOC, and satellites in the incorrect orbital plane. Finally, we found that the empirical orbit models, which were originally designed for precise orbit determination of GNSS satellites in circular orbits, provide fully appropriate results also for highly eccentric orbits with variable linear and angular velocities. 相似文献
10.
This paper outlines the motivation for Global Navigation Satellite System (GNSS) software receivers. Features of traditional
and software-based GNSS receiver architectures are highlighted and compared, focusing on the advantages of the software design.
The choice of which architecture is advantageous, particular in the case of embedded systems, is present along with design
criteria—both for the current environment as well as what can be expected in the future.
Electronic Publication 相似文献
11.
北斗三号卫星导航系统（BeiDou-3 navigation satellite system, BDS-3）已全面建成并向全球用户提供可靠的定位、导航和授时（positioning, navigation and timing, PNT）服务。为了实现与其他全球卫星导航系统（global navigation satellite system, GNSS）的兼容性和互操作性,BDS-3在BDS-2的基础上调制了B1C和B2a两个新信号,与伽利略系统（Galileo）的E1和E5a实现了频率的复用。系统间偏差（inter-system bias, ISB）对于实现不同GNSS之间的融合处理至关重要,为此提出了基于单差模型的ISB估计与应用算法,并对BDS-3与Galileo重叠频率之间的ISB进行了分析。基于可跟踪BDS-3新信号的几类接收机,揭示了BDS-3和Galileo之间的ISB的特性,在此基础上分析了BDS-3和Galileo组合的实时动态（real-time kinematic, RTK）定位性能。结果表明,基于相同类型的接收机B1C-E1和B2a-E5a之间是不存在ISB... 相似文献
12.
国际GNSS服务(IGS)提供的GPS综合产品被广泛应用于各种高精度科学研究中. 随着各国卫星导航系统的发展,亟需研究针对多系统全球卫星导航系统(GNSS)产品的综合策略. 由于卫星姿态与钟差相互耦合,综合钟差时额外考虑姿态改正将进一步提高综合产品精度,因此研究了一种顾及卫星姿态的GNSS钟差综合策略,改正姿态后GPS综合残差最大可减小80%. 对142个IGS测站进行精密单点定位(PPP)解算发现,综合产品比单个分析中心产品更加稳定,东(E)、北(N)、高(U)方向的动态定位精度最大可提升22.7%、16.7%和18.3%. 相对于未顾及姿态改正的综合产品,顾及姿态改正的综合产品的动态定位精度最大可提升65.3%. 相似文献
13.
目前尚无一种GNSS数据质量检测软件可以兼容RINEX格式第二版和第三版、同时兼容四大导航卫星系统,严重滞后于GNSS的发展。基于MATLAB语言研发了一种新的数据质量检测软件BQC,不仅可以处理单观测文件,还可以对多个观测文件进行批处理;可以输出四大导航卫星系统的卫星角度位置、多径误差、电离层延迟、载噪比和周跳等信息及统计报告,在批处理模式下还可对多观测文件的数据质量进行比对;与TEQC相比具有较强的兼容性、算法优越性和直观性。随着四大导航系统的逐步完善和RINEX格式第三版的推广使用,该软件将会为GNSS的建设成果检验工作提供一种有力的支撑工具。 相似文献
14.
多模全球导航卫星系统（Global Navigation Satellite System,GNSS）精密单点定位（precise point positioning,PPP）存在系统间偏差（inter-system bias,ISB）,构建了顾及系统间偏差的多模GNSS融合PPP算法,对多星座实验（the multi-GNSS experiment,MGEX）监测网中的7个测站观测数据进行静态解算,获得Galileo、GLONASS、北斗与全球定位系统之间的ISB值。分析结果表明,四系统PPP融合定位在水平分量和高程分量的精度分别为8.9 mm、5.3 mm和10.9 mm,体现出较高的融合定位精度。不同系统ISB值在单天内的稳定性较好,均优于0.12 ns。从多天ISB序列看,ISB存在不规律跳变,变化幅度可达近20 ns。不同类型接收机ISB存在一定差异,同一类型接收机结果相近。综合来看,Galileo ISB值最稳定且结果最优,北斗与GLONASS结果相当。 相似文献
15.
现阶段高轨道航天器导航主要依靠地基测控系统,为了研究全球卫星导航系统(GNSS)技术用于高轨道航天器导航的可行性,对GNSS技术在地球静止轨道(GEO)卫星、倾斜地球同步轨道(IGSO)卫星航天器中的导航精度及适用性展开了分析研究. 采用2021年11月9日的两行轨道数据(TLE)仿真GNSS星座,以不同星下点的GEO卫星和不同倾角的IGSO卫星作为目标星展开导航仿真试验. 实验结果表明:为了满足GNSS解算所需的卫星数量,须通过接收旁瓣信号来增加可见卫星数目. 对GEO目标星而言,当接收机灵敏度高于?169 dB时,导航精度可达30 m;利用GPS对7个不同的GEO或IGSO轨道目标星进行导航实验表明,GPS对目标星导航的位置误差约为35 m;北斗三号(BDS-3)、GPS、GLONASS、Galileo的导航位置误差均值分别为28.03 m、21.16 m、37.15 m、25.09 m,具有良好的内符合精度,其中GPS精度最高,GLONASS精度最低,但大部分时段也在45 m内. 相似文献
16.
17.
随着全球卫星导航系统(GNSS)的发展和移动通信技术的进步,用户对位置服务(LBS)提出了更高的要求. 本文采用市面上常见的两部Android智能手机采集GNSS数据,对Android智能手机伪距单点定位(SPP)和单频精密单点定位(PPP)算法进行研究,分析了在不同条件下智能手机的SPP、单频PPP定位性能. 结果表明:在使用多普勒平滑伪距和信噪比随机模型的基础上,Android智能手机GPS单系统的SPP定位精度可达3 m,GPS、Galileo、GLONASS、北斗卫星导航系统(BDS)四系统定位精度可达亚米级. 在单频PPP静态定位中,在GPS单系统下,定位精度仅能达到米级,且收敛时间较长;在GPS、Galileo、GLONASS、BDS四系统下,定位精度可达亚米级,且平面方向可在40 min内收敛. 在单频PPP动态定位中,手机的定位精度仅能达到米级. 相似文献
18.
全球导航卫星反射信号遥感GNSS-R(Global Navigation Satellite System Reflectometry)是近年来新兴的一个学科交叉研究领域。本文在调研分析国内外研究进展的基础上,基于GNSS-R工作原理与技术特征,将GNSS-R遥感观测模式定义为双天线模式DAP(Double Antenna Pattern)和单天线模式SAP(Single Antenna Pattern),并对两种观测模式的特性和共性问题进行分析。初步建立GNSS-R遥感应用体系架构,以陆面遥感应用为例,结合近几年参与的GNSS-R观测试验与模型研究工作,给出两种观测模式下GNSS-R遥感的典型应用实例,以期为中国未来地基、空基和星载GNSS-R遥感观测及应用工作的开展提供参考。 相似文献
19.
One of the key approaches to monitor the integrity of Global Satellite Navigation Systems (GNSS) is receiver autonomous integrity monitoring (RAIM). Existing RAIM algorithms utilise two tests in the position domain (for RAIM availability) and measurement domain (for failure detection). This paper proposes an alternative RAIM algorithm, which is based entirely in the measurement domain. This algorithm can be used for sensitivity analyses to support performance specification and system design. It can also be used during actual flight operations where the trigger is the phase of flight and its required navigation performance (RNP) parameters. This is made possible by computationally efficient calculation of the chi-squared parameters. The algorithm reverts to the current approach if the phase of flight is unknown. Simulation results for non-precision approach (NPA) have been used to demonstrate the effectiveness of the proposed algorithm. 相似文献