用于HALE无人机气象观测的小型高空成像仪和探测辐射计(CHAISR)微波辐射计初步试飞

R. K. Choi, J. Ha, Ki-Hoon Kim, Y. Cho, S. Joo, Do-Youn Kim, Seunghyun Min, Ho-Jin Lee, Seohoon Yang, Jongsung Park, Sanghyun Beck, Tae Gyu Kim
{"title":"用于HALE无人机气象观测的小型高空成像仪和探测辐射计(CHAISR)微波辐射计初步试飞","authors":"R. K. Choi, J. Ha, Ki-Hoon Kim, Y. Cho, S. Joo, Do-Youn Kim, Seunghyun Min, Ho-Jin Lee, Seohoon Yang, Jongsung Park, Sanghyun Beck, Tae Gyu Kim","doi":"10.1109/MICRORAD.2018.8430726","DOIUrl":null,"url":null,"abstract":"Three compact microwave radiometers are developed for a lightweight solar-powered HALE UAV (High-Altitude, Long Endurance; Unmanned Aerial Vehicle) or pseudo-satellite. The platform aims to operate at UTLS, i.e. altitude of 16~20 km, where air becomes thin enough to prevent operation of a conventional fossil fuel engines. Despite atmospheric science community has long been attracted in its potential scientific and operational value as an observation platform, only limited opportunities were available. The payload aims to obtain vertical temperature profiles and column-averaged water vapour for entire troposphere where most weather system takes place. Given total weight (< 3 kg) and maximum power (< 50 W) constraints are not the only challenges for design of the CHAISR. It requires nominal operation in thermal range between −75 and +43 °C and from 1013 to 50 hPa. Along with optical cameras and in situ sensors in the CHASIR, three microwave radiometers with 16 channels from 18 to 60 GHz are to fit in 130 mm diameter and 290 mm length with total weight less than 1.5 kg for cross-track scan unit. Maximum power consumption of less than 15 W does not allow conventional internal blackbody calibration facility onboard, and alternative methods has been developed. This study represents calibration of miniature microwave radiometer followed by preliminary results of a series of test flights conducted in 2017. While CHAISR has reached 2/3 of its target altitude, data from test flight showed effective performance of tipping curve calibration with altitude as expected. On the contrary, pre-flight calibration with liquid nitrogen indicates there are rooms to improve method of lab-based characterisation of the CHAISR. The result suggests feasibility of in situ cold reference for microwave radiometer and better than 1°K of total RMSE can be achievable once accuracy of warm reference is available from noise diode or ambient temperature readings. Continuous improvement of quality of instrument is currently explored at the same time, researching way of improving current specification of microwave radiometer in CHAISR.","PeriodicalId":423162,"journal":{"name":"2018 IEEE 15th Specialist Meeting on Microwave Radiometry and Remote Sensing of the Environment (MicroRad)","volume":"18 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2018-03-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"1","resultStr":"{\"title\":\"Preliminary Test Flight of a Compact High Altitude Imager and Sounding Radiometer (CHAISR) Microwave Radiometers for Meteorological Observation from HALE UAV\",\"authors\":\"R. K. Choi, J. Ha, Ki-Hoon Kim, Y. Cho, S. Joo, Do-Youn Kim, Seunghyun Min, Ho-Jin Lee, Seohoon Yang, Jongsung Park, Sanghyun Beck, Tae Gyu Kim\",\"doi\":\"10.1109/MICRORAD.2018.8430726\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"Three compact microwave radiometers are developed for a lightweight solar-powered HALE UAV (High-Altitude, Long Endurance; Unmanned Aerial Vehicle) or pseudo-satellite. The platform aims to operate at UTLS, i.e. altitude of 16~20 km, where air becomes thin enough to prevent operation of a conventional fossil fuel engines. Despite atmospheric science community has long been attracted in its potential scientific and operational value as an observation platform, only limited opportunities were available. The payload aims to obtain vertical temperature profiles and column-averaged water vapour for entire troposphere where most weather system takes place. Given total weight (< 3 kg) and maximum power (< 50 W) constraints are not the only challenges for design of the CHAISR. It requires nominal operation in thermal range between −75 and +43 °C and from 1013 to 50 hPa. Along with optical cameras and in situ sensors in the CHASIR, three microwave radiometers with 16 channels from 18 to 60 GHz are to fit in 130 mm diameter and 290 mm length with total weight less than 1.5 kg for cross-track scan unit. Maximum power consumption of less than 15 W does not allow conventional internal blackbody calibration facility onboard, and alternative methods has been developed. This study represents calibration of miniature microwave radiometer followed by preliminary results of a series of test flights conducted in 2017. While CHAISR has reached 2/3 of its target altitude, data from test flight showed effective performance of tipping curve calibration with altitude as expected. On the contrary, pre-flight calibration with liquid nitrogen indicates there are rooms to improve method of lab-based characterisation of the CHAISR. The result suggests feasibility of in situ cold reference for microwave radiometer and better than 1°K of total RMSE can be achievable once accuracy of warm reference is available from noise diode or ambient temperature readings. Continuous improvement of quality of instrument is currently explored at the same time, researching way of improving current specification of microwave radiometer in CHAISR.\",\"PeriodicalId\":423162,\"journal\":{\"name\":\"2018 IEEE 15th Specialist Meeting on Microwave Radiometry and Remote Sensing of the Environment (MicroRad)\",\"volume\":\"18 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2018-03-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"1\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2018 IEEE 15th Specialist Meeting on Microwave Radiometry and Remote Sensing of the Environment (MicroRad)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/MICRORAD.2018.8430726\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2018 IEEE 15th Specialist Meeting on Microwave Radiometry and Remote Sensing of the Environment (MicroRad)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/MICRORAD.2018.8430726","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 1

摘要

三台紧凑型微波辐射计用于轻型太阳能HALE无人机(高空,长航时;无人驾驶飞行器)或伪卫星。该平台的目标是在UTLS运行,即16~20公里的高度,那里的空气变得足够稀薄,无法运行传统的化石燃料发动机。尽管大气科学界长期以来一直被其作为观测平台的潜在科学和业务价值所吸引,但只有有限的机会。有效载荷旨在获得整个对流层的垂直温度分布和柱平均水蒸气,其中大多数天气系统发生。考虑到总重量(< 3 kg)和最大功率(< 50 W)的限制并不是CHAISR设计的唯一挑战。它的标称工作温度范围为- 75至+43°C, 1013至50 hPa。与光学摄像机和原位传感器一起,CHASIR中的三个微波辐射计具有16个通道,从18到60 GHz,适合直径130毫米,长度290毫米,总重量小于1.5公斤的交叉轨道扫描单元。最大功耗小于15w不允许传统的内部黑体校准设施机载,替代方法已经开发。该研究代表了微型微波辐射计的校准,随后是2017年进行的一系列试飞的初步结果。当CHAISR达到目标高度的2/3时,试飞数据显示,随着高度的变化,倾斜曲线的校准效果良好。相反,飞行前液氮校准表明,基于实验室的CHAISR表征方法还有改进的余地。结果表明,采用微波辐射计原位冷参比是可行的,只要噪声二极管或环境温度读数能提供精确的热参比,总均方根误差可达1°K以上。在探索不断提高仪器质量的同时,研究提高CHAISR微波辐射计电流指标的途径。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Preliminary Test Flight of a Compact High Altitude Imager and Sounding Radiometer (CHAISR) Microwave Radiometers for Meteorological Observation from HALE UAV
Three compact microwave radiometers are developed for a lightweight solar-powered HALE UAV (High-Altitude, Long Endurance; Unmanned Aerial Vehicle) or pseudo-satellite. The platform aims to operate at UTLS, i.e. altitude of 16~20 km, where air becomes thin enough to prevent operation of a conventional fossil fuel engines. Despite atmospheric science community has long been attracted in its potential scientific and operational value as an observation platform, only limited opportunities were available. The payload aims to obtain vertical temperature profiles and column-averaged water vapour for entire troposphere where most weather system takes place. Given total weight (< 3 kg) and maximum power (< 50 W) constraints are not the only challenges for design of the CHAISR. It requires nominal operation in thermal range between −75 and +43 °C and from 1013 to 50 hPa. Along with optical cameras and in situ sensors in the CHASIR, three microwave radiometers with 16 channels from 18 to 60 GHz are to fit in 130 mm diameter and 290 mm length with total weight less than 1.5 kg for cross-track scan unit. Maximum power consumption of less than 15 W does not allow conventional internal blackbody calibration facility onboard, and alternative methods has been developed. This study represents calibration of miniature microwave radiometer followed by preliminary results of a series of test flights conducted in 2017. While CHAISR has reached 2/3 of its target altitude, data from test flight showed effective performance of tipping curve calibration with altitude as expected. On the contrary, pre-flight calibration with liquid nitrogen indicates there are rooms to improve method of lab-based characterisation of the CHAISR. The result suggests feasibility of in situ cold reference for microwave radiometer and better than 1°K of total RMSE can be achievable once accuracy of warm reference is available from noise diode or ambient temperature readings. Continuous improvement of quality of instrument is currently explored at the same time, researching way of improving current specification of microwave radiometer in CHAISR.
求助全文
通过发布文献求助,成功后即可免费获取论文全文。 去求助
来源期刊
自引率
0.00%
发文量
0
×
引用
GB/T 7714-2015
复制
MLA
复制
APA
复制
导出至
BibTeX EndNote RefMan NoteFirst NoteExpress
×
提示
您的信息不完整,为了账户安全,请先补充。
现在去补充
×
提示
您因"违规操作"
具体请查看互助需知
我知道了
×
提示
确定
请完成安全验证×
copy
已复制链接
快去分享给好友吧!
我知道了
右上角分享
点击右上角分享
0
联系我们:info@booksci.cn Book学术提供免费学术资源搜索服务,方便国内外学者检索中英文文献。致力于提供最便捷和优质的服务体验。 Copyright © 2023 布克学术 All rights reserved.
京ICP备2023020795号-1
ghs 京公网安备 11010802042870号
Book学术文献互助
Book学术文献互助群
群 号:481959085
Book学术官方微信