GPS/GLONASS同步的可编程逻辑实现

给出了一种用于第三代移动通信系统(3G)CDMA2000基站的时钟同步方案。由一个双星接收卡接收GPS/GLONASS标准秒信号作为整个时钟同步系统的参考,分两级锁相环实现:第一级锁相环采用软件锁相,输出10MHz信号作为第二级锁相环的参考源,第二级锁相环为2个模拟锁相环,分别输出16fc和48fc(fc=1.2288MHz)。2S信号由16fc分频得到。这种设计保证了输出时钟的长期稳定性和短期稳定性,满足协议所规定的同步精度。详细介绍了数字鉴相器、2S产生电路、相差检测及控制电路的电路设计和有关仿真结果。     

基于GPS秒时钟的高精度同步时钟设计

限制通信定位技术发展的一个关键问题是时间同步。提出了一种用高精度晶振修正GPS秒时钟信号获取高精度同步时钟的新方法。     

CDMA2000基站时钟同步系统及电路

CDMA2000基站以GPS／GLONASS标准秒信号作为整个系统的时钟同步基准,采用一种PLL（锁相环）＋DDS（直接数字频率合成器）＋PLL的结构实现。引入了时钟同步系统的总体方案。着重介绍了由AD9851和LMX2306构成的后级DDS＋PLL的电路设计和参数设置。根据实验结果对该方案的稳定性和适用性进行了分析。     

单片机控制高性能时钟同步锁相环的实现与研究

本文介绍了单片机控制的高性能时钟同步锁相环的实现方法及性能特点，并简要阐述了其工作原理。在给出该锁相环数字模型的基础上，对锁相环控制软件算法进行分析，在频域给出了２种算法的分析结果，最后给出了主从同步锁相环的硬件测试结果。     

一种高精度GPS时间同步方案的应用

本文介绍了一种高精度GPS时间同步方案。通过分析卫星信号传输产生的误差,采用GPS双频接收技术和P—RTK数据处理技术实现了高精度时间同步,并且对设备同步结果进行了测试,满足了试验要求。     

一种快速提取位同步的全数字锁相环

本文提出了一种快速提取位同步的全数字锁相环方案。该方案通过对同步区、反相区以及快慢区的切换,有效地克服了同步时间与量化相位误差的矛盾。具有同步建立时间短、保持时间长、且同步精度高、抗干扰能力强等优点。     

利用GPS时钟及NTP实现广电网络时钟同步

随着广电系统双向网络改造的完成,视频类业务的多样化运营,广电系统网络中的相关设备对于时钟同步信息的需求越来越高。本文为了解决广电系统网络设备类型多样,设备分层架构组网的特点,基于广电系统接收GPS时钟作为精确时钟源的特点,使用NTP协议完成全网部署时钟源同步的方案。     

Combined GPS/GLONASS LAAS flight trials

The use of GPS in aviation is now accepted, with extensive work being undertaken on the technological, precision and infrastructure requirements. Work has focused on providing a service that is able to operate continuously in all areas. GPS alone, however, is seen as being unable to satisfy the stringent requirements for some phases of flight. Of the many solutions proposed, the Russian GLONASS system has been regularly overlooked. The research described in this paper aims to present GLONASS as a realistic and proven augmentation to GPS for aircraft positioning. During October 1996 the Civil Aviation Authority (CAA) Institute of Satellite Navigation (ISN) at the University of Leeds, in conjunction with the National Air Traffic Services Ltd (NATS UK) and the Defence Evaluation and Research Agency (DERA), performed a series of landmark differential GPS/GLONASS flight tests using the DERA BAC 1–11 flying laboratory. A real-time differential system was constructed using two GPS/GLONASS receivers developed by the ISN and a C-band data link for the RTCA corrections. Integration onboard the aircraft with avionic sensors and flight management systems was achieved using the ARINC 429 protocol. Routes were designed and flown to evaluate the complete system over a variety of airborne dynamics for both en-route and approach situations. In total, over 16 h of flying time was recorded, including 30 runway approaches over nine flights. A thorough evaluation of the accuracy and integrity of the positioning system was performed. Emphasis was made in comparing the flight statistics with recognized Required Navigation Performance (RNP) figures. The paper describes in detail the project development and the results achieved. An analysis of the results, showing that aircraft positioning with GPS/GLONASS augmentation in a local area augmentation system (LAAS) scenario can achieve accuracies that are both comparable with GPS-alone solutions and can satisfy up to CAT II precision approach criteria, is presented. Results are also given for position propagation using velocities derived from GPS and GLONASS carrier phase measurements. © 1997 John Wiley & Sons, Ltd.     

cdma2000-1x系统中GPS时钟算法

本文从一个简单、完善的自动机模型出发,介绍了一种正确获取GPS同步时钟的方法,并将其应用于cdma2000-1x系统中。数学推导表明,采用本文提供的算法获取的GPS同步时钟可以有效减少由于GPS时钟硬件的不稳定因素而造成的时钟精度损失,并能周期性地校正所取得的GPS时钟,控制时钟误差精度在100ns范围内。此算法实现简单,计算结果表明,该算法可以大幅度提高时钟精度。     

GPS/GLONASS/BDS三系统组合定位的定权方法

为了提高 GPS/GLONASS/BDS三系统组合定位的稳定性和精确度,研究加权最小二乘定位中的定权方法。提出一种结合高度角先验定权和验后方差估计的定权方法,利用多系统兼容接收机实测数据进行仿真验证。结果表明,相较于传统的最小二乘法,该定权方法可以明显改善多系统组合定位的精确度,且具有很好的抗差性能,提高了定位结果的稳定性,可应用于多系统兼容接收机组合定位解算中。     

Integrated GPS/GLONASS navigation: Algorithms and results

The presence of selective availability (SA) on GPS has led to a variety of proposals for mitigation of its effects, for example combining GPS with other sensors or by identifying and removing the SA using redundant information in the position solution. A further method for reducing the impact of SA is the combination of GPS and GLONASS measurements. GLONASS does not have any deliberate degradation. This paper describes several algorithms for combining GPS and GLONASS measurements in real time on a single receiver. There are two least squares solutions using the code phase measurements alone: one with the measurements from both systems weighted equally, and one with the measurements weighted by the covariance of the measurements. Kalman filters with no SA model, and first- and second-order models, using both the code and carrier phase to estimate user position and velocity, are also implemented. Two different adaptive schemes are compared which attempt to identify SA model parameters in real time. The algorithms are compared in terms of their positioning accuracy, computational overhead and robustness. A ten-channel GPS/GLONASS receiver developed at The University of Leeds is used to provide satellite data for the evaluation of the different methods.     

GPS接收机码/载波跟踪环技术及其抗干扰能力分析

为了提高GPS接收机的抗干扰能力，美国采取了一系列抗干扰技术措施，其中码／载波跟踪环技术是现代数字GPS接收机普遍采用的技术。本文主要通过分析数字GPS接收机的码／载波跟踪环技术，根据经验法则确定的载波跟踪环（PLL）与码跟踪延迟锁相环（DLL）门限，对采用码／载波跟踪环技术的GPS接收机的抗干扰能力进行分析。     

INS/GPS紧组合系统PLL最优带宽的选取

在INS/GPS紧组合系统中,通过INS提供的多普勒辅助信息可以消除GPS跟踪环路的动态性,同时降低环路带宽来抑制热噪声的影响,从而提高GPS系统的抗干扰能力。环路带宽是跟踪环路的一个重要参数,不能任意选取,当GPS跟踪环路设置为最优带宽时,系统性能将达到最优状态。为了保持系统性能最优,首先对影响最优带宽的各个误差源进行分析,提出了易于实现的迭代最优带宽算法,最后进行了仿真实验验证,结果表明在相同动态下采用最优带宽比固定带宽的系统具有更高的抗干扰能力和更强的跟踪锁定性能。     

基于自适应锁相环的高动态GPS信号载波跟踪算法

提出了一种基于四维卡尔曼滤波的自适应锁相环算法,并将该算法用于高动态GPS信号的载波跟踪.详细推导了卡尔曼滤波与数字锁相环之间的等效性,并给出了相应的环路更新步骤.仿真结果表明,该算法相对于采用固定增益数字锁相环的算法明显地降低了载波跟踪过程的均方根频率误差,提高了接收机的测速精度.     

一种高精度A／D转换电路

文章提出了一种利用ＭＣＳ－５１单片微机计算机构成的三斜式Ａ／Ｄ转换电路，其中讨论了Ａ／Ｄ转换电路的原理，最后，给出了可行的硬件电路及调试软件框架。