Methods of mutual high-precision navigation based the use of relative modes of anglemeasuring receivers of global navigation satellite systems signals

D. Dmitriev, V. N. Tyapkin, Y. Fateev, A. Gladyshev, N. S. Kremez
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Abstract

The article presents the results of experimental studies of mutual high-precision navigation methods for unmanned and specialized transport systems. The proposed methods are based on the application of the relative operating modes of two or more angle-measuring receivers of global navigation satellite systems signals. To conduct research, a software and hardware complex has been developed, consisting of two angle-measuring receivers of global navigation satellite systems signals, a turntable and a computer model of the navigation system of unmanned and specialized transport systems. It provides the positioning error of the antenna system in angular coordinates less than 1 arc minute, which allows it to be used as a reference when measuring the angular displacements of the receiver of global navigation satellite systems signals antenna system. The results of measurements of planar and angular coordinates both in autonomous and relative phase modes of operation of goniometric receivers global navigation satellite systems signals are presented and analyzed. It has been established that the root-mean-square error of measuring relative coordinates was 0,019 meter. A further increase in the relative position measurement accuracy is possible by taking measures to reduce the multipath reception error, which is the most significant uncorrelated position measurement error by two sets of receivers of global navigation satellite systems signals. Thus, the methods of mutual high-precision navigation using angle-measuring receivers of global navigation satellite systems signals have high accuracy without the use of external information about differential corrections. This will allow the operation of unmanned or special transport systems in hard-toreach and northern regions, in conditions of lack of communication and other adverse factors.
基于全球卫星导航系统信号测角接收机相对模式的相互高精度导航方法
本文介绍了无人运输系统与专用运输系统相互高精度导航方法的实验研究结果。所提出的方法是基于全球卫星导航系统信号的两个或多个测角接收机的相对工作模式的应用。为了进行研究,已经开发了一个软件和硬件综合体,包括两个全球导航卫星系统信号的角度测量接收器,一个转盘和一个无人驾驶和专门运输系统导航系统的计算机模型。它提供了天线系统在角坐标下的定位误差小于1角分,可以作为测量全球导航卫星系统信号天线系统接收机角位移的参考。给出并分析了全球卫星导航系统的平面坐标和角坐标在自主和相对相位两种工作模式下的测量结果。确定了相对坐标测量的均方根误差为0.019 m。多径接收误差是全球导航卫星系统两组接收机信号中最显著的不相关位置测量误差,通过采取措施减小多径接收误差,可以进一步提高相对位置测量精度。因此,利用全球卫星导航系统信号测角接收机进行互高精度导航的方法,在不使用外部差分改正信息的情况下,具有很高的精度。这将允许在缺乏通信和其他不利因素的条件下,在难以到达的北部地区运行无人驾驶或特殊运输系统。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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