GPS接收机精度特性的软件后处理方法

Abdellah El Abbous, N. Raissouni, A. Azyat, N. Samama
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引用次数: 1

摘要

本文以低成本GPS接收机的导航处理模块为研究对象,对GPS误差的表征和建模进行了研究。导航数据采用低成本的GPS接收天线进行记录,并采用RTKLIB c++封装的GPS后处理算法进行后处理。该方法允许我们研究和模拟单一定位模式下的误差变化。重点讨论了GPS误差的精度稀释度(DOP)特征,并通过软件后处理进行了计算。当使用良好的卫星几何形状时,DOP参数显示了GPS定位解决方案质量的良好指示。对于导航处理,通常选择DOP的最低值(DOP <;4)使GPS误差最小化。但通常,这是选择一些低海拔角度的卫星。解决这一问题的方法是选择最佳俯仰角和最佳俯仰角的最小DOP值。试验是使用固定天线接收器进行的,减少了多径等其他误差源的影响。在这种情况下,我们将使用所有卫星的性能与使用准最优算法生成的4颗卫星选择最佳几何形状进行了比较。将两者进行比较,计算星座的DOP和相应的接收机位置误差。结果表明,该方法能较好地处理最佳的卫星几何形状,得到较精确的DOP与误差之间的相关关系。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
A software post-processing method for GPS receiver's accuracy characterization
In this paper we focus on the navigation processing module of a low cost GPS receiver, in order to study the GPS errors characterization and modeling. The navigation data are recorded using a low cost GPS receiver antenna, and post-processed using GPS post-processing algorithms used in RTKLIB C++ package. This method allowed us to study and simulate errors variation in the case of a single positioning mode. An important focus was given to the Dilution of Precision (DOP) characterization of GPS errors, on the computed solution by a software post-processing. The DOP parameter showed a good indication of the quality of the GPS positioning solution, when using good satellite geometry. For navigation processing, it is usually convenient to choose the lowest value of DOP (DOP <; 4) in order to minimize the GPS errors. But often, this is to choose some satellites with low elevations angles. As a solution for this issue, the best case is obtained when choosing a minimum DOP with best and optimum elevation angle. The experience was carried out using a fixed antenna receiver, where the effects of other sources of errors such as multipath were reduced. In this case, we compare the performances of using all the satellites in view, to choosing the optimum geometry obtained using 4 satellites generated by a quasi-optimal algorithm. This two are employed to be compared and to calculate the constellation's DOP and the corresponding receiver's position error. Results show that it s better to deal with best satellites geometry, and an accurate correlation between DOP and resulting errors can be obtained.
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