GLONASS卫星广播星历精度分析

讨论了对GLONASS卫星广播星历进行误差分析采取的方案;通过对GLONASS广播星历与IAC分析中心精密星历与钟差产品的比较,分析了连续两周所有健康GLONASS卫星的广播星历轨道及钟差的误差特性。分析结果表明：当前GLONASS广播星历轨道误差的径向均方根误差在1 m以内,切向均方根误差在6 m以内,法向均方根误差在4 m以内,GLONASS钟差误差均方根误差在15 ns以内;从空间信号测距误差(SISRE)分析, GLONASS卫星广播星历整体精度优于4.5 m。     

基于BDS/GLONASS的短基线单历元多频RTK定位研究

在基于几何的TCAR(three carrier ambiguity resolution)算法基础上,将BDS/GLONASS组合引入到宽巷和窄巷模糊度解算中,提出一种基于双系统组合的单历元多频RTK定位模型,并通过实验进行分析。结果表明,相比于其他模型,该模型在模糊度解算效率和定位精度方面都是最优的。     

实时GLONASS精密卫星钟差估计及实时精密单点定位

研究非差实时GLONASS精密卫星钟差的估计方法,并将实时钟差应用于实时精密单点定位。采用自编软件,依据全球均匀分布的GNSS参考站实测数据,基于非差消电离层组合载波和伪距观测量,实现了GLONASS实时精密卫星钟差估计。实验结果表明,自主估计的实时GLONASS卫星钟差与ESA发布的最终精密钟差具有较好的一致性,互差优于0.5 ns|用于实时精密单点定位,能够获得静态定位cm 级精度,仿动态定位水平方向5~15 cm、高程方向10~30 cm的精度。     

基于精密星历的GPS／GLONASS组合单点定位研究

采用了俄罗斯空间局信息分析中心提供的GPS与GLONASS精密星历和钟差产品,处理了国际IGS站Dlft站的GPS／GLONAss双系统一整天观测数据,分析了所获得的可靠试验结果。     

GPS/GLONASS组合精密单点定位模型及结果分析

在GPS和GLONASS观测方程中考虑硬件延迟偏差的基础上,推导了GPS/GLONASS双系统组合精密单点定位的数学模型,并分析了硬件延迟偏差对估计的未知参数的影响。利用IGS跟踪站的观测数据和动态实验数据,对组合GPS/GLONASS精密单点定位模型进行了试算,并与GPS单系统精密单点定位的结果进行了比较。     

SLR资料精密测定GLONASS卫星轨道

将SLR资料计算的轨道与CODE轨道进行了比较,并将比较结果转换到RTN坐标系中。通过比较分析发现,两种轨道差值在轨道径向、法向和沿轨方向的精度分别优于10cm、50cm和45cm;SLR和微波资料确定的GLONASS卫星轨道在径向存在系统误差,该系统误差随卫星轨道面的不同而不同。     

GPS/GLONASS组合单点定位及精度分析

介绍了基于广播星历的GPS/GLONASS组合导航单点定位的数学模型,分析了组合导航的技术难点。在GPS伪距法单点定位的基础上进行组合导航定位,其中GLONASS卫星坐标运用四阶龙格—库塔(Runge-Kutta)数值积分方法求得,利用一种新的不需要进行轨道拟合的编程方法来进行计算。以IGS跟踪站提供的观测数据为例,分别采用GPS、GLO-NASS和GPS/GLONASS三种方式组合进行伪距法单点定位,同时比较分析了不同权重选择对组合定位精度的影响。     

GPS/GLONASS组合单点定位中选星算法的研究

通过分析影响定位精度的因素,给出了一种基于高度角和GDOP的组合选星算法,研究了其算法在GPS/GLONASS组合单点定位中的应用,在提高定位效率的同时提高了定位精度。结果表明,在动态定位中能快速选出较少的卫星组合用于定位解算,能满足动态用户对实时性的需求。     

Combined processing of the IGS and the IGEX network

 Since the beginning of the International Global Navigation Satellite System (GLONASS) Experiment, IGEX, in October 1998, the Center for Orbit Determination in Europe (CODE) has acted as an analysis center providing precise GLONASS orbits on a regular basis. In CODE's IGEX routine analysis the Global Positioning System (GPS) orbits and Earth rotation parameters are introduced as known quantities into the GLONASS processing. A new approach is studied, where data from the IGEX network are combined with GPS observations from the International GPS Service (IGS) network and all parameters (GPS and GLONASS orbits, Earth rotation parameters, and site coordinates) are estimated in one processing step. The influence of different solar radiation pressure parameterizations on the GLONASS orbits is studied using different parameter subsets of the extended CODE orbit model. Parameterization with three constant terms in the three orthogonal directions, D, Y, and X (D = direction satellite–Sun, Y = direction of the satellite's solar panel axis), and two periodic terms in the X-direction, proves to be adequate for GLONASS satellites. As a result of the processing it is found that the solar radiation pressure effect for the GLONASS satellites is significantly different in the Y-direction from that for the GPS satellites, and an extensive analysis is carried out to investigate the effect in detail. SLR observations from the ILRS network are used as an independent check on the quality of the GLONASS orbital solutions. Both processing aspects, combining the two networks and changing the orbit parameterization, significantly improve the quality of the determined GLONASS orbits compared to the orbits stemming from CODE's IGEX routine processing. Received: 10 May 2000 / Accepted: 9 October 2000     

GPS-assisted GLONASS orbit determination

 Using 1 week of data from a network of GPS/GLONASS dual-tracking receivers, 15-cm accurate GLONASS orbit determination is demonstrated with an approach that combines GPS and GLONASS data. GPS data are used to define the reference frame, synchronize receiver clocks and determine troposphere delay for the GLONASS tracking network. GLONASS tracking data are then processed separately, with the GPS-defined parameters held fixed, to determine the GLONASS orbit. The quality of the GLONASS orbit determination is currently limited by the size and distribution of the tracking network, and by the unavailability of a sufficiently refined solar pressure model. Temporal variations in the differential clock bias of the dual-tracking receivers are found to have secondary impact on the orbit determination accuracy. Received: 5 January 2000 / Accepted: 15 February 2001