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GNSS-BASED ATTITUDE DETERMINATION ALGORITHM AND TRIPLE-ANTENNA GNSS RECEIVER FOR ITS IMPLEMENTATION

机译:基于GNSS的姿态确定算法和三天线GNSS接收器的实现。

摘要

An algorithm for determining of a vehicle orientation based on a coherent processing of GNSS signals received by three spaced antennas and a special GNSS receiver for implementing this algorithm are considered. The three antennas are logically combined into two pairs, with one of the antennas becoming common for both pairs. The GNSS receiver measures the first carrier phase difference between the signals received within each pair of antennas. The first differences of the full phases are represented as the sum of an integer number of periods of the carrier frequency and the fractional part of the period. Values of the fractional parts of the first differences are used to compute the orientation of the vector connecting the antennas phase centers within each pair. The use of the fractional parts of the first differences makes it possible to exclude the integer ambiguity resolution in carrier phase measurements. The attitude of the vehicle is calculated from the orientation of two non-collinear vectors with a common origin, measured by two pairs of antennas. In the special GNSS receiver for the vehicles attitude measurements, each antenna is connected to its own RF front end. All RF front ends, heterodynes, digital navigation processors of this receiver are clocked from one common clock oscillator. In this case, all the carrier phase measurements of the GNSS signals received by the three spaced antennas are performed and processed coherently, i.e. in a common time scale.
机译:考虑了一种基于三个间隔天线接收的GNSS信号的相干处理来确定车辆方向的算法,以及用于实现该算法的特殊GNSS接收器。三个天线在逻辑上合并为两对,其中一对天线共用。 GNSS接收机测量每对天线中接收到的信号之间的第一载波相位差。全相位的第一差表示为载波频率的整数个周期与该周期的分数部分之和。第一差的小数部分的值用于计算每对中连接天线相位中心的矢量的方向。通过使用第一差的小数部分,可以排除载波相位测量中的整数歧义分辨率。车辆的姿态是根据两个非共线矢量的方向(由两对天线测量)得出的,该矢量具有相同的原点。在用于车辆姿态测量的特殊GNSS接收器中,每个天线都连接到其自己的RF前端。该接收器的所有RF前端,外差,数字导航处理器均由一个公共时钟振荡器提供时钟。在这种情况下,由三个隔开的天线接收的GNSS信号的所有载波相位测量都是相干地,即在共同的时间尺度上进行和处理的。

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