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罗兰C时差信号测量误差是影响定位精度的关键。简要介绍了罗兰C系统的定位原理和卡尔曼滤波技术,针对罗兰C时差信号的特征,设计卡尔曼滤波算法,基于CV模型和CA模型分别对罗兰C静态定位和动态定位的实测数据进行处理,得出相关结论,具有一定的工程实用意义。 相似文献
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为了降低卫星导航的使用风险,美国和一些导航大国都积极加强其陆基无线电导航系统特别是罗兰C系统的进一步研究。这说明在开发应用卫星导航系统的同时,还必须继续发展陆基无线电导航系统。因此,我国在大力发展双星导航系统的同时,还应继续加强罗兰C系统的研究,积极开发双星/罗兰C组合导航的潜力。对双星/罗兰C组合导航技术的数据组合方法进行介绍,比较了不同组合方式的导航精度及工作性能。 相似文献
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河南省农村集体土地建设用地和宅基地使用权调查已逐步开始,全省统一布设D,E级GPS控制网作为农村集体土地使用权调查的基础控制,采用国家A,B级GPS点和河南省C级GPS点作为起算数据。本文阐述各地级市的市区、县域建立农村集体土地使用权调查坐标系统的方法和采用的起算数据及与历史地籍资料坐标系统的转换原理与方法。 相似文献
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应用GPS技术,在四川中东部地区进行了C级GPS网的布设。结合GPS网的布设及数据处理方法,介绍了GPS技术应用于C级GPS网施测中的作业方法和体会。 相似文献
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窄带干扰(NBI)是罗兰C接收机接收信号中普遍存在的一种干扰。这种窄带干扰经常淹没有用的罗兰C信号,因此,去掉NBI对罗兰C接收机的正常工作尤为重要。分别采用最小均方误差(LMS)自适应算法和二阶自适应格型滤波器算法对带有窄带干扰的罗兰C信号进行处理。仿真结果得出:LMS自适应滤波器对同步干扰和近同步干扰都有很好的效果;但是由于罗兰C信号本身的编码信息而比较难获取期望信号,加上LMS自适应滤波器实现阶数较高,实现相对困难。二阶格型自适应滤波器由于是完全除去干扰频率点,不能用于同步干扰,但其对近同步干扰和非同步干扰仍然有很好的效果,且其实现较为简单,易于在工程上应用。 相似文献
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针对低信噪比条件下,罗兰C天波信号延迟时间估计的准确性和有效性问题,提出基于优化包络的相关系数时域法。通过分析标准罗兰C信号包络的特征,分别采用微分和二次微分方法对罗兰C信号包络进行优化,形成陡峭的包络信号上升沿;利用相关系数法对接收信号包络和参考信号包络进行匹配,形成的匹配峰值分别对应地波和天波信号到达的时刻,由此可获得天波信号的延迟时间;通过仿真分析和实测信号试验验证,证明该方法能满足数字化接收机的实际要求,并具有更高的抗干扰能力、估计准确性和自动识别功能的特点。估计的结果还可以作为判别相位跟踪和周期识别正确率的辅助依据。 相似文献
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罗兰C系统常用单台链双曲线算法进行定位.我国台站的分布导致定位精度下降,为了改善台站分布对精度的影响,对罗兰C交叉台链双曲线的几何精度因子(GDOP)算法进行了推导.并运用MATIAB工具仿真了南海(16°N,107°E)到(25°N,118°E)区域的几何定位因子分布.对单台链和交叉台链算法的几何精度因子进行了对比,... 相似文献
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增强型罗兰导航系统(eLoran)作为全球卫星导航系统(GNSS)的备份系统,是国家定位导航授时(PNT)安全的重要基础设施.针对目前标准eLoran信号存在易受交叉干扰、天波干扰,通信数据传输速率低等的问题,本文基于标准罗兰信号体制提出了两种波形改进方法(衰减函数法与对称波形法)并对新型波形进行性能评估.实验结果表明,两种方法能够有效缩短波形持续时间,加速后沿波形下降,减小发射机功耗.对称波形法能够大幅减小波形持续时间,但缩短波形持续时间也将改变原信号波形的频谱特性,利用衰减函数法可以最大程度保证信号的频谱性能.综合分析可知,新型波形能够有效利用时域资源,空余的时间可用于增加传输信号,进而提高数据调制技术的性能. 相似文献
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针对罗兰-C无线电导航信号接收需求,研究一种高性能的罗兰-C小型有源接收天线,可以减小天线体积和安装难度,方便罗兰-C导航接收机的使用,具有较高的实用意义. 天线主体采用磁棒线圈天线接收长波频段罗兰-C信号,在天线内设计了包含放大电路、带通滤波电路、差分输出电路和供电电路在内的前端信号调理电路,从而增大信号灵敏度,提高信噪比;设计了一体化的天线结构,以便工程化应用. 通过仿真和实测结果表明:该天线在工作频带内,可以全向高效接收罗兰-C信号,而且对接收到的微弱罗兰-C信号进行放大并滤除带外噪声,信号强度和信噪比满足使用要求. 该天线具有体积小、灵敏度高、使用方便的特点,可应用于罗兰-C无线电导航,组合导航、附加二次相位时延计算等场景. 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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As the battle environment becomes more complicated, the demand for higher accuracy and better anti-jam capacity of navigation has been increasing. The conventional JTIDS/INS/GPS integrated navigation cannot meet the demands of certain situations such as precision strike and formation flight. A new system that introduces the differential GPS into JTIDS/INS/GPS integration system is proposed to improve the navigation performance in the modern combined operations. In this system, the differential information of DGPS is transmitted through the communication data link of Link-16. As a result, the system resources are efficiently utilized and the controllability and anti-jam performance of the system are significantly enhanced. A hybrid slot allocation protocol (HSAP) that combines a static slot allocation algorithm and a dynamic slot allocation algorithm and the corresponding source-chosen mechanisms are proposed. The performance of the JTIDS/INS/GPS integration navigation using the differential GPS information from one or multiple base stations is studied and compared with that of the system without using the differential GPS information. Furthermore, the performance of the integration navigation using HSAP is compared with that of the system using static slot allocation algorithm. We show that navigation accuracy based on the differential GPS is improved, and using HSAP also leads to higher localization accuracy. 相似文献
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Discussion of GPS Anti-Jam Technology 总被引:4,自引:0,他引:4
The Global Positioning System (GPS) satellita navigation aiding system, sometimes called NAVSTAR, has become a utility to
the military and many civilian areas. GPS, currently consisting of 24 satellites, is used by the military for navigation,
precision weapons delivery, and the future digital battlefield. In the civilian sector, GPS is widely used as the primary
or secondary aid for land, water, and air navigation; as a surveying aid; as a vehicle location system; and as a precision
time standard for cellular and ATM sites. In the aviation community, GPS is becoming an integral part of the WAAS (Wide Area
Augmentation System) and the LAAS (Local Area Augmentation System) for en route navigation in North America and Category II
and III precision approach, and for surface navigation. The vulnerability of GPS have become the vulnerabilities of WAAS and
LAAS, and require consideration of interference mittigation techniques. ? 1999 John Wiley & Sons, Inc. 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
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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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