惯性导航 姿态角等的计算和输出 得到分的积分低飞偶发-INS attitude angles so calculated and output by occasional low-flying points points

惯性导航测试程序，根据输入的六轴传感器信号，机型轨迹重建-Inertial navigation test procedures, according to the six-axis sensor input signal, the model trajectory reconstruction