某型飞机导航软件参数处理的研究

Research on the Parameter Smooth Process of Navigation Software for Certain Type of Airplane

在分析某型飞机导航软件时发现 ,该软件在计算位置、航向等参数校正量时要引入相应的系数 ,根据原始资料中的控制结构图 ,对位置校正量进行了详细的研究 ,结果表明 :该软件对位置校正量采用了惯性环节进行平滑 ,其方法能够有效的抑制校正过程出现的干扰。

During the study of navigation software for certain type of airplane, it is found that the corresponding coefficient is brought to correct the value of position and heading. According to the control figure of the original information, the correct value of position is analyzed in detail, it is concluded that the correct value is smoothed with inertial ring in software, and this mehod can effectively restrain the disturbance in the correct process and can be used as a reference.