结合加速度计零位和标度因数的温度误差模型，采用了相应的误差补偿算法。
The proper error-compensation method is adopted based on the temperature error model of the accelerometer.
针对平面拦截问题，选择导弹和目标之间的相对速度矢量与导弹-目标视线之间的夹角（称为相对航向误差角）作为将要被控制到零的输出。
For the case of planar interception, the so called relative heading error angle between the relative velocity vector and the LoS (Line of Sight) is chosen as the output to be controlled to zero.
在数据分析方面，利用VB6.0语言编程进行处理，大大提高了测量轴孔类零件尺寸及其误差的计算精度和运算速度。
In analyzing the data, the speed and accuracy of calculation about the size and errors of the shaft and hole parts is raised highly by using VB6.0 programming.
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