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ERROR COMPENSATION OF TEMPERATURE DEVIATIONS IN BAROMETRICALLY SUPPORTED INERTIA SENSOR SYSTEMS

机译:气压支撑惯性传感器系统中温度偏差的误差补偿

摘要

A method for error compensation of temperature deviations in barometrically supported inertia sensor systems, in which measured values of acceleration are collected (10) and optionally suitably transformed, and a corresponding acceleration signal is produced and integrated (20) once for producing a signal representing a geodetic vertical speed (GVS), said acceleration signal being integrated (30) a second time for producing a signal indicating the elevation (IFBA), wherein the obtained signal indicating the elevation is matched (82) to an elevation value obtained from barometric measurement of a normalized standard atmosphere (HSTDBARO). The error compensation comprises producing a correction parameter representing a function of the deviation of the actual temperature (STT) from the standard temperature at the corresponding elevation, and the respective correction parameter representing the temperature deviation is applied to the signal produced from the acceleration measurements in the vertical direction (vert accel; GVS; IFBA) so that speed and position values (BVS; IFBA; IFBAPC) arise which nearly correspond to a barometric elevation signal.
机译:一种在气压支持下的惯性传感器系统中对温度偏差进行误差补偿的方法,其中收集加速度的测量值(10)并进行适当的转换,然后生成一次相应的加速度信号并将其积分(20),以产生表示加速度的信号。大地垂直速度(GVS),所述加速度信号第二次被积分(30)以产生指示高程(IFBA)的信号,其中所获得的指示高程的信号与从气压测量得到的高程值相匹配(82)。标准化标准大气(HSTDBARO)。误差补偿包括产生表示实际温度(STT)与相应高度处的标准温度的偏差的函数的校正参数,并且将表示温度偏差的各个校正参数应用于由加速度测量产生的信号。垂直方向(垂直加速度; GVS; IFBA),以便产生速度和位置值(BVS; IFBA; IFBAPC),这些值几乎对应于气压高程信号。

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