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A Direct Attitude Determination Approach Based on GPS Double-Difference Carrier Phase Measurements

机译:GPS双差分载波相位测量的直接姿态确定方法

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摘要

The principle of the traditional attitude solution approach based on GPS (Global Position System) is to get the attitude matrix according to the relationship of coordinates. During the progress, the error of baseline position assumed in ECEF (Earth-Centered Earth-Fixed) and the error of coordinate transform between body frame and reference frame (ENU, East-North-Up) have been included in the result, and finally the precision of attitude determination is reduced. This contribution presents a new approach of attitude determination, in which the attitude angles are calculated by the double-difference carrier phase equation of GPS according to the relationship of attitude matrix and attitude angles through least-squares estimate method. The new approach predigests the procedure of attitude determination which reduces the error assumed. According to the analysis the precision of attitude determination is higher than that of traditional method. It is shown it gets a precise attitude result with the direct attitude determination method in the simulation. A novel algorithm is proposed to solve some problems. Simulation results show the effectiveness of the proposed algorithm.
机译:传统的基于GPS(全球定位系统)的姿态求解方法的原理是根据坐标的关系获得姿态矩阵。在此过程中,结果包括了ECEF(以地球为中心的地球固定)中假定的基线位置误差以及车身框架与参考框架之间的坐标变换误差(ENU,东北向上)姿态确定的精度降低。该贡献提出了一种姿态确定的新方法,该方法通过最小二乘估计法根据姿态矩阵与姿态角之间的关系,通过GPS的双差载波相位方程来计算姿态角。新方法简化了姿态确定的过程,从而减少了假定的误差。分析表明,姿态确定的精度高于传统方法。结果表明,采用直接姿态确定方法可以得到精确的姿态结果。提出了一种新颖的算法来解决一些问题。仿真结果表明了该算法的有效性。

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