Department of Biosystems and Agricultural Engineering, University of Kentucky, Lexington, KY 40546, USA.
Applied Statistics Laboratory, University of Kentucky, Lexington, KY 40546, USA.
Sensors (Basel). 2022 Apr 24;22(9):3261. doi: 10.3390/s22093261.
Small unmanned aircraft systems (UAS) are increasingly being used for meteorology and atmospheric monitoring. The ease of deployment makes distributed sensing of parameters such as barometric pressure, temperature, and relative humidity in the lower atmospheric boundary layer feasible. However, constraints on payload size and weight, and to a lesser extent power, limit the types of sensors that can be deployed. The objective of this work was to develop a miniature pressure-temperature-humidity (PTH) probe for UAS integration. A set of eight PTH probes were fabricated and calibrated/validated using an environmental chamber. An automated routine was developed to facilitate calibration and validation from a large set of temperature and relative humidity setpoints. Linear regression was used to apply temperature and relative humidity calibrations. Barometric pressure was calibrated using a 1-point method consisting of an offset. The resulting PTH probes were less than 4 g in mass and consumed less than 1 mA when operated from a 5 VDC source. Measurements were transmitted as a formatted string in ASCII format at 1 Hz over a 3.3 V TTL UART. Prior to calibration, measurements between individual PTH probes were significantly different. After calibration, no significant differences in temperature measurements across all PTH probes were observed, and the level of significance between PTH probes was reduced. Actual differences between calibrated PTH probes were likely to be negligible for most UAS-based applications, regardless of significance. RMSE across all calibrated PTH probes for the pressure, temperature, and relative humidity was less than 31 Pa, 0.13 °C, and 0.8% RH, respectively. The resulting calibrated PTH probes will improve the ability to quantify small variations in ambient conditions during coordinated multi-UAS flights.
小型无人机系统(UAS)越来越多地用于气象和大气监测。由于易于部署,可以实现对低层大气边界层中参数(如气压、温度和相对湿度)的分布式感测。然而,由于有效负载大小和重量的限制,以及在较小程度上的功率限制,限制了可以部署的传感器类型。这项工作的目的是开发一种用于 UAS 集成的微型压力-温度-湿度(PTH)探头。制作了一组八个 PTH 探头,并使用环境室对其进行了校准/验证。开发了一种自动化例程,以便从大量温度和相对湿度设定点方便地进行校准和验证。线性回归用于应用温度和相对湿度校准。气压通过包含偏移量的单点法进行校准。最终的 PTH 探头的质量小于 4 克,并且从 5 VDC 源运行时消耗的电流小于 1 mA。测量值以 ASCII 格式在 3.3 V TTL UART 上以 1 Hz 的速率传输为格式化字符串。在进行校准之前,各个 PTH 探头之间的测量值差异显著。在进行校准之后,所有 PTH 探头的温度测量值之间没有观察到显著差异,并且 PTH 探头之间的显着性水平降低。对于大多数基于 UAS 的应用程序,无论显着性如何,校准后的 PTH 探头之间的实际差异可能可以忽略不计。所有校准后的 PTH 探头的压力、温度和相对湿度的 RMSE 分别小于 31 Pa、0.13°C 和 0.8%RH。校准后的 PTH 探头将提高在协调多架 UAS 飞行期间量化环境条件小变化的能力。