Quality evaluation for measurements of wind field and turbulent fluxes from a UAV-based eddy covariance system

被引:2
|
作者
Sun, Yibo [1 ,2 ,3 ]
Sude, Bilige [1 ,2 ,3 ]
Lin, Xingwen [4 ]
Geng, Bing [5 ]
Liu, Bo [1 ,2 ,3 ]
Ji, Shengnan [1 ,2 ,3 ]
Jing, Junping [6 ]
Zhu, Zhiping [7 ,8 ]
Xu, Ziwei [9 ]
Liu, Shaomin [9 ]
Quan, Zhanjun [1 ,2 ,3 ]
机构
[1] Chinese Res Inst Environm Sci, State Key Lab Environm Criteria & Risk Assessment, Beijing 100012, Peoples R China
[2] Chinese Res Inst Environm Sci, Inst Ecol, Beijing 100012, Peoples R China
[3] State Environm Protect Key Lab Ecol Reg Proc & Fu, Beijing 100012, Peoples R China
[4] Zhejiang Normal Univ, Coll Geog & Environm Sci, Jinhua 321004, Peoples R China
[5] Beijing Acad Social Sci, Beijing 100101, Peoples R China
[6] Natl Ocean Technol Ctr, Tianjin 300112, Peoples R China
[7] China Geol Survey, Kunming Gen Survey Nat Resources Ctr, Kunming 650111, Peoples R China
[8] Minist Nat Resources, Technol Innovat Ctr Nat Ecosyst Carbon Sink, Kunming 650100, Peoples R China
[9] Beijing Normal Univ, Fac Geog Sci, State Key Lab Earth Surface Proc & Resource Ecol, Beijing 100875, Peoples R China
基金
中国国家自然科学基金;
关键词
UNMANNED AIRCRAFT; WATER-VAPOR; CO2; FLUX; AIRBORNE; EVAPOTRANSPIRATION; UNCERTAINTY; ENERGY; CONSEQUENCES; VARIABILITY; CALIBRATION;
D O I
10.5194/amt-16-5659-2023
中图分类号
P4 [大气科学(气象学)];
学科分类号
0706 ; 070601 ;
摘要
Instrumentation packages for eddy covariance (EC) measurements have been developed for unoccupied aerial vehicles (UAVs) to measure the turbulent fluxes of latent heat ( L E ), sensible heat ( H ), and CO 2 ( F c ) in the atmospheric boundary layer. This study aims to evaluate the performance of this UAV-based EC system. First, the measurement precision ( 1 sigma ) of georeferenced wind was estimated to be 0.07 m s - 1 . Then, the effect of the calibration parameter and aerodynamic characteristics of the UAV on wind measurement was examined by conducting a set of calibration flights. The results showed that the calibration improved the quality of the measured wind field, and the influence of upwash and the leverage effect can be ignored in wind measurement by the UAV. Third, for the measurements of turbulent fluxes, the error caused by instrumental noise was estimated to be 0.03 mu mol m - 2 s - 1 for F c , 0.02 W m - 2 for H , and 0.08 W m - 2 for L E . Fourth, data from the standard operational flights were used to assess the influence of resonance on the measurements and to test the sensitivity of the measurement under the variation ( +/- 30 %) in the calibration parameters around their optimum value. The results showed that the effect of resonance mainly affected the measurement of CO 2 ( similar to 5 %). The pitch offset angle ( epsilon theta ) significantly affected the measurement of vertical wind ( similar to 30 %) and turbulent fluxes ( similar to 15 %). The heading offset angle ( epsilon psi ) mainly affected the measurement of horizontal wind ( similar to 15 %), and other calibration parameters had no significant effect on the measurements. The results lend confidence to the use of the UAV-based EC system and suggest future improvements for the optimization of the next-generation system.
引用
收藏
页码:5659 / 5679
页数:21
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