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Calibrating airborne measurements of airspeed, pressure and temperature using a Doppler laser air-motion sensor

机译:使用多普勒激光空气运动传感器校准空速,压力和温度的机载测量

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A new laser air-motion sensor measures the true airspeed with a standard uncertainty of less than 0.1 m s−1 and so reduces uncertainty in the measured component of the relative wind along the longitudinal axis of the aircraft to about the same level. The calculated pressure expected from that airspeed at the inlet of a pitot tube then provides a basis for calibrating the measurements of dynamic and static pressure, reducing standard uncertainty in those measurements to less than 0.3 hPa and the precision applicable to steady flight conditions to about 0.1 hPa. These improved measurements of pressure, combined with high-resolution measurements of geometric altitude from the global positioning system, then indicate (via integrations of the hydrostatic equation during climbs and descents) that the offset and uncertainty in temperature measurement for one research aircraft are +0.3 ± 0.3 °C. For airspeed, pressure and temperature, these are significant reductions in uncertainty vs. those obtained from calibrations using standard techniques. Finally, it is shown that although the initial calibration of the measured static and dynamic pressures requires a measured temperature, once calibrated these measured pressures and the measurement of airspeed from the new laser air-motion sensor provide a measurement of temperature that does not depend on any other temperature sensor.
机译:新型的激光空气运动传感器以小于0.1 ms -1 的标准不确定度测量真实的空速,从而将沿飞机纵轴的相对风的测量分量的不确定度降低到大约同一级别。然后,从皮托管入口处的空速获得的预计压力将为校准动压和静压的测量提供基础,从而将这些测量中的标准不确定性降低到小于0.3 hPa,并将稳定飞行条件下的精度降低到约0.1 hPa。 hPa。这些改进的压力测量结果与来自全球定位系统的高分辨率几何高度测量结果相结合(然后通过爬升和下降过程中的静液压方程积分)表明,一架研究飞机的温度测量值的偏差和不确定度为+0.3 ±0.3°C。对于空速,压力和温度,与使用标准技术从标定中获得的不确定性相比,这些显着降低了不确定性。最后,表明尽管对测得的静态和动态压力的初始校准需要一个测得的温度,但是一旦校准了这些测得的压力以及来自新的激光空气运动传感器的空速的测量,就提供了不依赖于温度的测量值任何其他温度传感器。

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