基于矢量跟踪的GNSS／SINS相干深组合系统研究

为满足组合导航系统在高动态环境下的性能要求,设计基于矢量跟踪的GNSS／SINS相干深组合导航方法。利用矢量跟踪环路将所有可视卫星的跟踪和导航解算融为一体,增强通道间的辅助;高动态对载波跟踪影响更大,在通道预滤波中将码环载波环分别用独立的滤波器处理,组合滤波中采用通道间差分降低滤波状态维数,提高计算效率。引入惯导的加速度辅助本地信号参数预测,较精确地测量卫星视线方向的加速度,减小接收机在高动态时段的剩余动态,提高本地信号参数的预测精度。基于矢量跟踪软件接收机搭建相干深组合仿真系统,实验表明该方法在高动态等环境下能提高信号跟踪性能,改善系统的精度、可靠性。      

基于GPS软件接收机的SINS／GPS紧组合系统仿真

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。     

BDS/GPS单频软件接收机算法研究与实现

随着卫星导航定位技术及接收机的发展,软件接收机已成为当前研究的热点之一。根据北斗卫星导航定位系统（BDS）的接口控制文档（ICD）,分析了BDS B1I信号,提出了一种基于并行码相位和并行频率捕获的算法,实现了对BDS-B1I/GPS信号的捕获跟踪、导航电文解码。利用HG-SOFTGPS02采集器采集的数据进行BDS/GPS定位,验证了该算法的可行性与合理性。     

中频数据卫星捕获算法研究

软件无线电技术在卫星导航接收机中的应用在很大程度上改变了基带信号的处理方法.本文详细论述了基于FFT的频域快速捕获技术,通过对实测中频数据实验分析,指出仅利用门限方法无法准确在频域判决可视卫星,必须依靠其他信息进行辅助判决.在分析通过实测数据获得的可视卫星在连续扩频码周期内多普勒和伪码相位变化规律的基础上,给出了采用多...     

基于SIC的伪卫星系统抗远近效应捕获算法研究

地基伪卫星系统中由于远近效应的影响,近场伪卫星信号可能对远场伪卫星信号形成压制干扰,导致远场伪卫星信号无法被捕获. 针对该系统中使用的跳时直接序列扩频(TH-DSSS)信号的捕获问题,引入串行干扰消除(SIC)技术,缓解伪卫星系统中的远近效应问题,通过本地重构强信号和干扰对消降低强信号对弱信号捕获的影响,并从理论和仿真两方面对其性能进行了分析. 仿真结果表明,相比传统未采用干扰消除的捕获算法而言,基于SIC的信号捕获方法在不改变伪卫星基站结构和接收机框架的基础上,可有效降低远近效应的影响,提高弱信号捕获概率,扩大系统工作范围,从而为接收机在强远近效应场景下的捕获、跟踪和定位解算提供有效保障.      

弱GPS/GLONASS信号捕获算法研究

本文给出了GPS/GLONASS双模接收机的总体设计方案,重点对弱信号环境下的接收机信号捕获进行了讨论,采用并行码相位搜索方法和改进的循环相关算法分别对GLONASS信号和GPS信号进行捕获;并利用真实数据对双模接收机性能进行了仿真研究,重点对接收机捕获弱信号的能力,以及在不同信噪比和不同累加数据长度下的捕获概率进行了讨论,结果表明该双模接收机在不需要较长数据长度的情况下能够捕获低信噪比环境下的卫星导航信号,提高了接收机的灵敏度。     

频域叠加的大频偏导航信号捕获算法

在卫星导航接收机的设计和实现过程中,信号捕获是卫星信号同步的关键步骤。只有捕获到了正确的相位和多普勒信息,才能初始化跟踪环路,进而完成信号的同步。针对高动态接收机在大频偏条件下实现信号捕获需要进行多次频域搜索,计算量成倍增加的问题,该文以GPS系统为例,分析了多普勒频偏对相关峰的影响,利用频域叠加技术设计了在多普勒频移过大条件下的信号捕获方案。分析结果表明,该捕获方案可以完成大频偏下的信号捕获,降低了多次频域搜索带来的计算量,并且具有较好的捕获性能。     

基于GPS单频软件接收机的捕获与跟踪算法实现

在分析基于软件无线电全球定位系统（GPS）接收机结构的基础上,研究了GPS单频软件接收机的捕获和跟踪算法,并基于MATLAB平台在PC上仿真了GPS单频软件接收机样机。信号捕获采用基于快速傅里叶变换（FFT）的并行码相位搜捕算法;信号跟踪联合使用超前滞后非相干延迟锁定环和科斯塔斯环的跟踪环结构。采用实测数据对信号捕获、跟踪算法进行了分析和验证。结果表明：仿真的GPS单频软件接收机具备基本的基带信号处理功能。     

GPS信号跟踪的多径影响分析与仿真

多径信号是GPS定位的主要误差源之一。码和载波跟踪环是GPS接收机的重要组成部分，它们直接决定了接收机的性能，因此当前多径消除技术研究的核心即是从跟踪环内部着手研究。本文仔细分析了GPS接收机信号跟踪环以及多径信号对跟踪精度的影响，对伪距码与载波相位多径误差进行了比较，并且通过仿真结果和图表阐明了码和载波相位多径误差之间的协同关系。     

GNSS导航信号的开环补偿多径抑制方法

多径的存在会给全球导航卫星系统的接收机带来较大的定位误差。因此,高精度的接收机须对多径信号进行抑制。针对目前常用的多径抑制方法的优缺点,提出了一种基于多门延迟和曲线拟合的多径抑制方法。该方法通过多门延迟来重塑伪码的自相关函数,用于找到直射信号的伪码真实位置和接收机码跟踪环路鉴别结果之间的偏差,进一步通过曲线拟合方法更加精确地计算出该偏差,最后将该偏差通过开环方法补偿给伪距计算,使得接收机在不改变环路跟踪性能和抗动态干扰性能的前提下实现定位性能的提升。仿真结果表明新算法在前端带宽的影响下对短、中长多径均能进行有效地抑制。      

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.     

圆周移位在伪码补零BDS信号捕获算法中的应用

D1导航电文中加入了NH码,且D2导航电文的速率也比GPS信号的快很多,使得BDS的信号结构增加了捕获难度。采用伪码补零的方法可以对BDS信号进行有效捕获,但是该方法积分时间较长导致捕获耗时变长。本文提出了一种基于圆周移位的改进伪码补零算法,将搜索中复杂的载波剥离运算用计算量很小的频谱序列的搬移操作来代替,使算法复杂度大幅下降。试验结果表明,该方法可以有效减少运算量和捕获耗时。     

TJS-2 geostationary satellite orbit determination using onboard GPS measurements

This study analyzes the quality of onboard data of tracking signals from GPS satellites on the far side of the earth and determines the orbit of the geostationary satellite using code and carrier phase observations with 30-h and 3-day orbit arc length. According to the analysis results, the onboard receiver can track 6–8 GPS satellites, and the minimum and maximum carrier to noise spectral densities were 24 and 45 dB-Hz, respectively. For a GPS receiver on a high-altitude platform above the navigation constellations, the blocking of the earth and a weak signal strength usually cause a piece-wise GPS signal tracking and an increase in the number of ambiguity parameters. Individual GPS satellites may be continuously tracked for as little as several minutes and as long as 3 h. Moreover, considering the negative sign of elevation angles reflects the fact that GPS satellites are tracked below the receiver in the study. GPS satellites appear mainly in the elevation angle range of ??53° to ??83°, and dilution of precision values could reach ten or one hundred and more. Also, it is observed that when a signal suffers from atmospheric refraction, other GPS signals tracked simultaneously by the receiver experience strong systematic errors in the code observations. Based on single-frequency code and carrier phase measurements, the mean 3D root mean square (RMS) value of the overlap comparisons between 30-h orbit determination arcs is 2.14 m. However, we found that there were also some biases in the carrier phase residuals, which contributed to poor orbit accuracy. To eliminate the effects of the biases, we established a correction sequence for each GPS satellite. After corrections, the mean 3D RMS was reduced to 0.99 m, representing a 53% improvement.     

GPS卫星信号Doppler频移的计算与分析

在GPS导航定位系统中，多普勒频率偏移直接影响接收机性能。为了克服多普勒频率偏移的影响，提高接收机的GPS信号捕获速度，对多普勒频移估计算法进行研究。通过分析可视卫星的判定、Doppler频移计算方法，基于NewStar150GPS原理实验平台，使用C＋＋语言编程，开发Doppler频移计算程序。实验结果表明，Doppler频移的大小与a有关。当a〈90°时，多普勒频移为正，用户接收机收到的频率比卫星发射的频率要低。当a〉90°时，多普勒频移为负；当a=90°时，多普勒频移为0。     

GPS与Galileo共用的MBOC信号研究

介绍了GPS与Galileo共用信号的演变过程，通过BOC（1，1）在兼容性、互操作性方面的表现，以及将MBOC（6，1，1／11）与之相比较，描述了MBOC（6，1，1／11）在这两个方面的表现。可供我国卫星导航信号体制设计借鉴学习，为GPS／Galileo接收机设计提供参考。     

A scheme for weak GPS signal acquisition aided by SINS information

In order to enhance the acquisition performance of global positioning system (GPS) receivers in weak signal conditions, a high-sensitivity acquisition scheme aided by strapdown inertial navigation system (SINS) information is proposed. The carrier Doppler shift and Doppler rate are pre-estimated with SINS aiding and GPS ephemeris, so that the frequency search space is reduced, and the dynamic effect on the acquisition sensitivity is mitigated effectively. Meanwhile, to eliminate the signal-to-noise ratio gain attenuation caused by data bit transitions, an optimal estimation of the unknown data bits is implemented with the Viterbi algorithm. A differential correction method is then utilized to improve the acquisition accuracy of Doppler shift and therefore to meet the requirement of carrier-tracking loop initialization. Finally, the reacquisition experiments of weak GPS signals are implemented in short signal blockage situations. The simulation results show that the proposed scheme can significantly improve the acquisition accuracy and sensitivity and shorten the reacquisition time.