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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 vehicle's 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信号的相干处理确定车辆取向的算法,以及用于实现该算法的特殊GNSS接收器。三个天线在逻辑上组合成两对,其中一个天线成为两对的常见。 GNSS接收器测量在每对天线内接收的信号之间的第一载波相位差。完整阶段的第一差异表示为载波频率的整数周期和周期的分数部分的总和。第一差异的分数部分的值用于计算连接天线阶段中心内的矢量的方向。第一差异的分数部分的使用使得可以在载波相位测量中排除整数模糊分辨率。从具有共同原点的两个非共线载体的方向计算车辆的姿态,由两对天线测量。在用于车辆姿态测量的特殊GNSS接收器中,每个天线连接到其自己的RF前端。所有RF前端,外司,该接收器的数字导航处理器从一个公共时钟振荡器时钟。在这种情况下,通过三个间隔天线接收的GNSS信号的所有载波相位测量,并连续地处理和处理,即在常规时间尺度。

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