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Research on Initial Precision Alignment Method of Strapdown Inertial Navigation System

机译:截头惯性导航系统初始精密对准方法研究

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According to the requirement of high precision initial alignment for Strapdown Inertial navigation, the precision alignment principle of strapdown inertial navigation is studied. Based on zero-speed as external information benchmark, a mathematical model of precision alignment based on Kalman filter is established, which mainly includes the state space model and measurement model of precision alignment, and the simulation experiments under static benchmark are carried out. The experimental results show that the precision alignment method studied is adopted for attitude determination. The error of pitch angle is reduced from 20'to less than 1', the error of roll angle is reduced from 15' to less than 1', and the error of course angle is reduced from 25'to less than 1'. The corresponding alignment time is 10s, 5S and 100s respectively, and the alignment time of course angle is longer.
机译:根据高精度初始对准的要求进行轴承型惯性导航,研究了泰拉斯特惯性导航的精密对准原理。基于零速作为外部信息基准,建立了基于卡尔曼滤波器的精密对准的数学模型,其主要包括状态空间模型和精密对准的测量模型,并执行静态基准下的仿真实验。实验结果表明,采用了研究的精确对准方法进行姿态测定。俯仰角的误差从20'TO减小到小于1',滚角的误差从15'变为小于1',并且当然角度的误差从小于1'的25'to减小。相应的对准时间分别为10s,5s和100s,并且当然角度的对准时间更长。

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