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The Research on Nonlinear Attitude Determination Method of GNSS Multi-antenna Attitude Measurement

机译:GNSS多天线姿态测量的非线性姿态确定方法研究

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GNSS multiple antenna attitude measurement possesses three attitude determination methods, direct solution, nonlinear least squares method and linear least squares method. Normal nonlinear least squares method on attitude estimate realizes linearization of observation equation with additive euler angle error being the parameter, of which the calculation is largely increased and accuracy can be further enhanced. Hence, nonlinear least squares methods respectively based on additive quaternion error, multiplicative euler angle error and multiplicative quaternion error are derived, and detailed calculation procedures and least squares solutions are respectively presented. Finally a simulation experiment is designed to compare and analyze the direct solution, linear least squares method and 4 types of nonlinear least squares method. Conclusions are as follows: (1) direct solution possesses short calculation time consumption, only being available to degree-level navigation application due to low accuracy; (2) the least squares method whose accuracy is higher than direct solution by more than 60%, reaching to 30', and single epoch time consumption is just a little more than direct solution, is available to minute-level navigation application; (3) nonlinear least squares method based on multiplicative error is relatively the best.
机译:GNSS多天线姿态测量具有三种姿态确定方法:直接解法,非线性最小二乘法和线性最小二乘法。正常的姿态估计非线性最小二乘法实现了以加性欧拉角误差为参数的观测方程的线性化,大大增加了计算量,可以进一步提高精度。因此,推导了分别基于加性四元数误差,乘性欧拉角误差和乘性四元数误差的非线性最小二乘法,并给出了详细的计算过程和最小二乘解。最后设计了一个仿真实验,对直接解法,线性最小二乘法和四种非线性最小二乘法进行比较和分析。结论如下:(1)直接解法计算时间短,精度低,仅适用于学位级导航应用。 (2)最小二乘方法的精度比直接解法高出60%以上,达到30',单历元时间消耗仅比直接解法稍多,可用于分钟级导航应用; (3)基于乘法误差的非线性最小二乘法相对最佳。

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