共查询到19条相似文献，搜索用时 156 毫秒
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组织实施了连续一周的渤海湾船载动态GPS定位试验,对BNC软件客户端接收的IGS实时数据流4种综合产品(IGC01、IGS01、IGS02和IGS03)的数据可用性和精度进行了验证;对基于RTS改正的船载实时精密单点定位的精度进行了分析。结果表明,4种RTS产品的数据可用率均在90%以上,其中IGS01的数据可用率最高为97.68%;以IGS最终精密星历和钟差产品为参考,4种RTS轨道产品在X、Y、Z方向的精度(RMS)均优于4cm,钟差产品的精度(STD)优于0.2ns;以采用IGS最终精密星历和钟差产品的事后PPP结果为参考,基于RTS的船载RTPPP的水平方向精度优于7cm,高程方向精度为12cm,三维位置精度约为15cm。 相似文献
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在已有后处理精密单点定位Fortran程序的基础上,基于C/C++和Fortran的混合编程技术,实现了实时静态精密单点定位,其中高精度卫星轨道及钟差参数由卫星广播星历和SSR改正信息数据流实时估算,卫星观测数据流由GNSS接收机实时提供。通过实时精密单点定位程序验证了混合编程技术的可行性,对于相关的研究工作和精密单点定位的实时性应用具有参考价值。GPS单系统实时静态精密单点定位试验结果表明:在6 h观测时段,1 s采样间隔的情况下,实时静态精密单点定位的收敛时间约为30~100 min;利用实时定位解算结果与测站精确坐标求差计算的RMS,收敛后可实现水平方向优于5 cm,垂直方向优于10 cm。 相似文献
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在GPS单点定位和相对定位中都需要不断计算卫星的坐标。IGS提供的精密星历为15min间隔，要得到更小间隔的数据，就要进行插值。利用广义延拓插值进行GPS精密星历插值，探讨插值精度与三个参数的关系，并与Lagrange多项式插值和三角插值结果进行比较。结果表明，广义延拓插值法具有较高的精度，完全适用于精密星历的插值。 相似文献
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目前IGS共提供6类精度和时效性不同的精密星历产品,为了验证不同精度和时效性的IGS精密星历产品在海洋测绘中的适用情况,使用6类不同的IGS精密星历产品,分别对固定点观测数据和海上浮动点观测数据进行精密单点定位解算,并对解算结果分别进行比对分析和统计。固定点比对结果表明,IGS和IGR精密星历精密单点定位解算在平面位置方向均能达到平均8厘米的外符合精度,IGU00至IGU18精密单点定位解算精度稍差,平面外符合精度在10～13cm,且精度随着发布时间的推迟而提高;PPP潮位的解算结果表明,从IGS至IGU18,高程方向的解算精度相当,和固定潮位站的数据相比,均方根差在16～18cm。 相似文献
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常规精密单点定位实时反演水汽,存在精度低或稳定性差等问题,因此提出了一种基于参考站改正信息的PPP实时水汽反演方法。首先利用参考站的天顶对流层延迟解算观测值改正信息,然后对流动站共视卫星的观测值进行误差改正,利用IGU预报星历和钟差产品,采用PPP算法进行实时水汽反演。以中国香港HKSC为流动站,分别选取中国台湾TWTF和中国香港HKWS作为参考站,开展参考站辅助的PPP实时水汽反演试验。结果表明,分别以无线电探空数据和ECMWF数据为参考,本方法4个时段的平均标准差分别为1.9 mm和2.9 mm;相比基于IGU的常规PPP实时水汽反演方法,精度分别提升60%和51%。本方法参考站的选择不受距离限制,精度与使用IGS事后精密星历的PPP水汽反演基本一致,相比常规PPP和相对定位方式的实时水汽反演具有明显优势。 相似文献
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研究了单频GPS精密单点定位的算法,包括单频精密单点定位的回归方程及卡尔曼滤波用于单频精密单点定位,探讨卡尔曼滤波的观测方程和状态方程,给出了状态转移矩阵及系统噪声矩阵.通过算例验证了在1s采样率的情况下,定位达到了分米级的精度. 相似文献
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The IGS Real-time Pilot Project (IGS-RTPP) provides real-time precise orbits and clocks, which support real-time positioning for single stations over large areas using the Precise Point Positioning (PPP) technique. This paper investigates the impact of real-time orbits, network configuration, and analysis strategies on real-time PPP implementation and demonstrates the real-time PPP performance. One month of data from the IGS network is analyzed in a real-time simulation mode. Results reveal the following: (1) In clock estimation, differential approaches are much more efficient than the zero-differenced approach. (2) The precision of IGS Ultra rapid (IGU) orbits could meet the IGS-RTPP requirement for precise clock estimation and PPP positioning. (3) Considering efficiency and precision, a network with 50 stations is recommended for the IGS-RTPP. It is demonstrated that the real-time satellite clock precision is 0.1 ns supporting hourly static PPP with a mean precision of 2–3 cm in the North component and 3–4 cm in the other components. Kinematic PPP assessed with onboard GPS data collected from a buoy provided mean coordinate precision of 2.2, 4.2, 6.1 cm in the North, East and Up directions, compared to the RTK solutions. 相似文献
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Y. Gao 《Marine Geodesy》2013,36(4):279-288
Global positioning system (GPS) has found applications in various areas including marine geodesy. GPS positioning accuracy, however, is greatly degraded by GPS ephemeris and clock errors, particularly errors due to Selective Availability (SA). Thus, it is crucial to use precise ephemeris and clock corrections for users who require high position accuracy. Presently, precise ephemeris and clock corrections are available only in post‐mission. This paper investigates the generation of precise real‐time ephemeris and clock corrections and the positioning accuracy using them. In this research, precise real‐time ephemeris is generated from accurate dynamic orbit prediction and clock corrections are calculated using instantaneous GPS measurements. Numerical analysis using data from an actual GPS tracking network is performed that indicates use of precise ephemeris and clock corrections can improve the positioning accuracy to the one meter level. This accuracy is attainable in real‐time as the precise real‐time ephemeris and clock corrections become available in the future. 相似文献
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海洋一号C/D（HY-1C/D）卫星中国海洋水色水温扫描仪（Chinese Ocean Color and Temperature Scanner,COCTS）主要用于探测海洋水色、水温等要素,这些要素需要经过卫星资料处理才能获取,而几何定位是预处理的核心,直接影响这些要素的质量。COCTS具有114°视场角和四元逐点摆扫的特征,据此研究出一套完整的几何定位方法。从0级数据中提取卫星星历,利用插值法从中获取采样时间对应的卫星位置和速度,进而得到轨道（ORB）坐标系到地心旋转（ECR）坐标系的转换矩阵。基于四元逐点摆扫的特征,中心视矢量分别绕X轴、Y轴旋转相应角度,获得扫描行各采样点ORB视矢量,建立视矢量与地球交叉点关系模型,从而对根据波段数据绘制的遥感图像进行地理定位。本文使用插值法替代了传统需要6个轨道根数来计算卫星位置的复杂方法,同时直接计算ORB到ECR的转换矩阵,而不采用传统的两步转换方法。经过多组数据计算及定性定量验证,HY-1C/D COCTS几何定位结果一致;采样像元尺度效应导致从星下点到两侧边缘、从赤道到两极,误差逐渐增大,约在两个像元内。该方法满足一定的定位精度要求,可以用于COCTS的几何定位。 相似文献
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The French Transportable Laser Ranging System (FTLRS) was deployed in the calibration site of satellite radar altimeters in Corsica over the 2002 and 2005 campaigns. The paper describes the different steps of SLR data processing. The average arcs RMS obtained are about 1–2 cm for Lageos-1&;-2, Starlette and Stella satellites; it is shown that the best results of satellite orbits determination and geocentric positioning are obtained with Eigen-Grace03s gravity model. The difference of FTLRS absolute 3D positioning, between 2002 and 2005, of about 7.7 mm (i.e., 2.6 mm/yr) is less than residual errors of ITRF2005 velocities (of about 4.3 mm/yr). 相似文献
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Precise, long-range GPS kinematic positioning to centimeter accuracy requires that carrier phase ambiguities be resolved correctly during an initialization period, and subsequently to recover the “lost" ambiguities in the event of a cycle slip. Furthermore, to maximize navigational efficiency, ambiguity resolution and carrier phase-based positioning need to be carried out in real-time. Due to the presence of the ionospheric signal delay, satellite orbit errors, and the tropospheric delay, so-called absolute ambiguity resolution “on-the-fly” for long-range applications becomes very difficult, and largely impossible. However, all of these errors exhibit a high degree of spatial and temporal correlation. In the case of short-range ambiguity resolution, because of the high spatial correlation, their effect can be neglected, but their influence will dramatically increase as the baseline length increases. On the other hand, between discrete trajectory epochs, they will still exhibit a large degree of similarity for short time spans. In this article, a method is described in which similar triple-differenced observables formed between one epoch with unknown ambiguities and another epoch with fixed ambiguities can be used to derive relative ambiguity values, which are ordinarily equal to zero (or to the number of cycles that have slipped when loss-of-lock occurred). Because of the temporal correlation characteristics of the error sources, the cycle slips can be recovered using the proposed methodology. In order to test the performance of this algorithm an experiment involving the precise positioning of an aircraft, over distances ranging from a few hundred meters up to 700 kilometres, was carried out. The results indicate that the proposed technique can successfully resolve relative ambiguities (or cycle slips) over long distances in an efficient manner that can be implemented in real-time. 相似文献