在惯性导航系统中，惯性元件的标度因数误差对系统的误差产生了极大的影响。
The scale-factor error of inertia component is greatly influential to the precision of Inertial Navigation System (INS).
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.
光纤陀螺与温度相关误差项主要为零漂和标度因数，输入轴失准角也是影响光纤陀螺应用的一个重要误差项。
The errors of FOG involved with temperature are zero bias and scale factor. Input axis misalignment is another important error with temperature.
光纤陀螺与温度相关误差项主要为零漂和标度因数，输入轴失准角也是影响光纤陀螺应用的一个重要误差项。
The errors of FOG involved with temperature are zero bias and scale factor. Input axis misalignment is another important error with temperature.
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