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FY-3E掩星反演电离层foF2、hmF2和TEC参数精度评估
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作者 蒋春华 安前芳 +2 位作者 李敏 祝会忠 刘广盛 《大地测量与地球动力学》 CSCD 北大核心 2024年第10期1010-1015,共6页
在分析FY-3E提供的每日掩星数据数量及其全球分布特征基础上,利用电离层垂测仪数据获取的F2层临界频率值(foF2)和F2层峰值高度(hmF2)、高精度全球电离层格网(GIM)及国际参考电离层模型(IRI2016)提供的总电子含量(TEC)对FY-3E掩星反演的f... 在分析FY-3E提供的每日掩星数据数量及其全球分布特征基础上,利用电离层垂测仪数据获取的F2层临界频率值(foF2)和F2层峰值高度(hmF2)、高精度全球电离层格网(GIM)及国际参考电离层模型(IRI2016)提供的总电子含量(TEC)对FY-3E掩星反演的foF2、hmF2和TEC精度进行评估。结果表明,电离层垂测仪和FY-3E反演的foF2和hmF2数据的相关系数分别为0.86和0.75,RMSE分别为0.99 MHz和19.26 km。以GIM数据获取的TEC为参考,FY-3E GPS和北斗(BDS)数据反演的TEC精度大致相当。FY-3E TEC精度与太阳活动呈负相关;FY-3E TEC与GIM TEC的相关系数为0.90,RMSE为5.23 TECu。FY-3E TEC与同高度范围的IRI2016 TEC的相关系数为0.88,RMSE为3.70 TECu。 展开更多
关键词 fy-3e F2层峰值参数 TeC GIM IRI2016 精度评估
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新息增量法评估FY-3E/HIRAS-Ⅱ观测质量
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作者 陈宏涛 官莉 《红外与毫米波学报》 SCIE EI CSCD 北大核心 2023年第6期834-844,共11页
FY-3E/HIRAS-Ⅱ作为世界上第一个晨昏轨道的星载红外高光谱仪器,评估其观测资料质量对提高资料同化分析场和全球数值天气预报精度具有十分重要的作用。本文基于2021年12月-2022年1月及2022年3月共35天的HIRAS-Ⅱ观测,采用新息增量法检... FY-3E/HIRAS-Ⅱ作为世界上第一个晨昏轨道的星载红外高光谱仪器,评估其观测资料质量对提高资料同化分析场和全球数值天气预报精度具有十分重要的作用。本文基于2021年12月-2022年1月及2022年3月共35天的HIRAS-Ⅱ观测,采用新息增量法检验了其在轨辐射观测资料质量,按陆地和洋面分别统计了O-B偏差和标准差的分布特征;进一步匹配相同时间段、相同区域的MetOp-B/IASI观测资料,使用双重差异的O-B法分析了HIRAS-Ⅱ观测资料质量,可消除偏差中辐射传输模式模拟的影响。结果表明,不论海洋还是陆地,HIRAS-Ⅱ长波与中波大部分通道的O-B平均偏差均小于0.5 K、标准差在1 K以内,陆地上标准差比洋面偏大(尤其是窗区通道)。664~665 cm^(-1)CO_(2)吸收带和1300~1680 cm^(-1)水汽吸收带,由于再分析资料的偏差引起RTTOV模拟的辐射值存在系统性误差,使得偏差较大;980~1080 cm^(-1)O_(3)吸收带和1300 cm^(-1)CH_(4)吸收带附近较大的偏差是由于辐射传输模式RTTOV中吸收气体浓度采用固定的气候廓线值造成的,这些波段与MetOp-B/IASI相比的double O-B偏差均趋近于0 K,说明O-B偏差主要是由于辐射传输模式模拟误差造成的,而不是仪器观测的质量低。短波大部分通道的O-B平均偏差在-2 K~2 K之间,标准差在2 K以内。1920 cm^(-1)附近通道由于是仪器中波与短波的交界处,采用的探测器不同造成较大的O-B偏差。2267~2380 cm^(-1)较大的偏差是由于RTTOV模拟亮温时没有考虑非局地热力平衡NLTE效应的影响。波数大于2400 cm^(-1)的短波波段由于太阳污染使得偏差和标准差都逐渐增大。HIRAS-ⅡO-B偏差随扫描角存在不对称现象,使用时需要进行扫描角偏差订正。 展开更多
关键词 fy-3e/HIRAS-Ⅱ RTTOV 新息增量法 观测质量评估
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FY-3E:The First Operational Meteorological Satellite Mission in an Early Morning Orbit 被引量:19
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作者 Peng ZHANG Xiuqing HU +5 位作者 Qifeng LU Aijun ZHU Manyun LIN Ling SUN Lin CHEN Na XU 《Advances in Atmospheric Sciences》 SCIE CAS CSCD 2022年第1期1-8,共8页
Fengyun-3 E(FY-3E),the world’s first early-morning-orbit meteorological satellite for civil use,was launched successfully at the Jiuquan Satellite Launch Center on 5 July 2021.The FY-3E satellite will fill the vacanc... Fengyun-3 E(FY-3E),the world’s first early-morning-orbit meteorological satellite for civil use,was launched successfully at the Jiuquan Satellite Launch Center on 5 July 2021.The FY-3E satellite will fill the vacancy of the global early-morning-orbit satellite observation,working together with the FY-3C and FY-3D satellites to achieve the data coverage of early morning,morning,and afternoon orbits.The combination of these three satellites will provide global data coverage for numerical weather prediction(NWP)at 6-hour intervals,effectively improving the accuracy and time efficiency of global NWP,which is of great significance to perfect the global earth observing system.In this article,the background and meteorological requirements for the early-morning-orbit satellite are reviewed,and the specifications of the FY-3E satellite,as well as the characteristics of the onboard instrumentation for earth observations,are also introduced.In addition,the ground segment and the retrieved geophysical products are also presented.It is believed that the NWP communities will significantly benefit from an optimal temporal distribution of observations provided by the early morning,mid-morning,and afternoon satellite missions.Further benefits are expected in numerous applications such as the monitoring of severe weather/climate events,the development of improved sampling designs of the diurnal cycle for accurate climate data records,more efficient monitoring of air quality by thermal infrared remote sensing,and the quasicontinuous monitoring of the sun for space weather and climate. 展开更多
关键词 fy-3e operational meteorological satellite early morning orbit
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Impact of Atmospheric Transmittance and NLTE Correction on Simulation of High Spectral Infrared Atmospheric Sounder onboard FY-3E
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作者 Chenggege FANG Peiming DONG +1 位作者 Yang HAN Wanlin KAN 《Journal of Meteorological Research》 SCIE CSCD 2024年第2期225-234,共10页
With the launch of the first civilian early-morning orbit satellite Fengyun-3E(FY-3E),higher demands are placed on the accuracy of radiative transfer simulations for hyperspectral infrared data.Therefore,several key i... With the launch of the first civilian early-morning orbit satellite Fengyun-3E(FY-3E),higher demands are placed on the accuracy of radiative transfer simulations for hyperspectral infrared data.Therefore,several key issues are investigated in the paper.First,the accuracy of the fast atmospheric transmittance model implemented in the Advanced Research and Modeling System(ARMS)has been evaluated with both the line-by-line radiative transfer model(LBLRTM)and the actual satellite observations.The results indicate that the biases are generally less than 0.25 K when compared to the LBLRTM,while below 1.0 K for the majority of the channels when compared to the observations.However,during both comparisons,significant biases are observed in certain channels.The accuracy of Hyperspectral Infrared Atmospheric Sounder-II(HIRAS-II)onboard FY-3E is comparable to,and even superior to that of the Cross-track Infrared Sounder(CrIS)onboard NOAA-20.Furthermore,apodization is a crucial step in the processing of hyperspectral data in that the apodization function is utilized as the instrument channel spectral response function to produce the satellite channel-averaged transmittance.To further explore the difference between the apodized and unapodized simulations,Sinc function is adopted in the fast transmittance model.It is found that the use of Sinc function can make the simulations fit the original satellite observations better.When simulating with apodized observations,the use of Sinc function exhibits larger deviations compared to the Hamming function.Moreover,a correction module is applied to minimize the impact of Non-Local Thermodynamic Equilibrium(NLTE)in the shortwave infrared band.It is verified that the implementation of the NLTE correction model leads to a significant reduction in the bias between the simulation and observation for this band. 展开更多
关键词 high spectral infrared sounding atmospheric transmittance APODIZATION Non-Local Thermodynamic equilibrium Fengyun-3e(fy-3e)
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FY-3E微波湿度计发射前定标的非线性系数在星上定标中的适用性分析 被引量:1
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作者 王振占 肖雨伟 +2 位作者 张升伟 何杰颖 谷松岩 《遥感学报》 EI CSCD 北大核心 2023年第10期2327-2336,共10页
星载微波湿度计发射前定标和在轨定标的最大不同是冷源的使用:在轨定标的冷源是宇宙冷空背景温度,通常为2.7 K,而发射前定标的冷源通常控制在80—100 K。这样通过发射前定标得到的非线性系数是否可以用于在轨定标一直是一个非常关心和... 星载微波湿度计发射前定标和在轨定标的最大不同是冷源的使用:在轨定标的冷源是宇宙冷空背景温度,通常为2.7 K,而发射前定标的冷源通常控制在80—100 K。这样通过发射前定标得到的非线性系数是否可以用于在轨定标一直是一个非常关心和值得研究的问题。本文通过在FY-3E微波湿度计发射前热真空定标中除了传统需要的冷热、变温定标源之外,另外设计了一个独立的位于180—200 K附近的定标源。利用该验证源,本文提出了三点定标公式,基于冷空不变性并通过外推到冷空亮温的模拟观测计算非线性系数。随后通过比较传统和新型非线性系数推导方法的结果,并将两组系数带入同一组数据中分析两组发射前定标系数用于在轨定标的适用性。结论表明,通过对传统方法和新方法的计算结果比较,发现将两组非线性方法应用于同一数据集的结果存在差异,说明传统方法得到的发射前系数存在误差。并且该方法简化了发射前标定过程,提高了非线性系数用于星上标定的精度。 展开更多
关键词 微波湿度计定标 fy-3微波湿度计 发射前定标 在轨定标 非线性系数
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风云三号E星中能质子探测器标定
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作者 郝梦坛 张珅毅 +7 位作者 侯东辉 沈国红 张焕新 苏波 白超平 孙莹 周平 冀文涛 《空间科学学报》 CAS CSCD 北大核心 2023年第3期558-566,共9页
风云三号E星搭载的中能质子探测器实现了风云三号系列卫星首次对辐射带中能质子进行多方向的测量。中能质子探测器实现了对九个方向的测量能量范围为0.03~5 MeV的中能质子能谱的测量。为确定中能质子探测器的实际性能,在仪器交付前,利... 风云三号E星搭载的中能质子探测器实现了风云三号系列卫星首次对辐射带中能质子进行多方向的测量。中能质子探测器实现了对九个方向的测量能量范围为0.03~5 MeV的中能质子能谱的测量。为确定中能质子探测器的实际性能,在仪器交付前,利用中国科学院国家空间科学中心的中高能电子加速器,对中能质子探测器的能量分辨率,相对响应效率曲线、不同方向探头测量一致性以及抗电子污染能力进行了标定。文中介绍了仪器的标定场所、标定内容,并对标定的结果做了分析。其结果显示,仪器的能量分辨率为6.50%@310 keV,各测量一致性偏差优于1.51%,电子在仪器内产生污染计数的概率低于1%。该结果为中能质子探测器在轨运行时数据的分析处理提供了重要的参考依据。 展开更多
关键词 太阳同步轨道 风云三号e 中能质子探测器 定标 能量分辨率
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AC vector magnetometer for space-based applications using low-resource magneto-impedance sensor
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作者 YU XiangQian HUANG Cong +14 位作者 XIAO ChiJie LI JiaWei LIU Si WANG JingDong LI YunPeng QU YaNan WANG YongFu CHEN HongFei ZOU Hong SHI WeiHong ZONG QiuGang CHEN XiaoFei ZHANG XiaoXin ZONG WeiGuo WANG JingSong 《Science China(Technological Sciences)》 SCIE EI CAS CSCD 2023年第12期3663-3670,共8页
This study proposes a novel AC vector magnetometer developed using a low-resource magneto-impedance sensor for China’s Feng-Yun meteorological satellite(FY-3E).It was calibrated and characterized to determine its per... This study proposes a novel AC vector magnetometer developed using a low-resource magneto-impedance sensor for China’s Feng-Yun meteorological satellite(FY-3E).It was calibrated and characterized to determine its performance parameters.The total weight of the AC vector magnetometer is 51 g(the aluminum box excluded),while the total power consumption is 310 m W.The proposed AC vector magnetometer can detect magnetic field variations in the range of±1000 nT and noise power spectral density of≤50 pT/Hz^(1/2)@1 Hz.Furthermore,the proposed device has a maximum nonlinearity of≤0.71‰over the entire range and a nonorthogonality error of 3.07 nT or 0.15%(root mean square).The total dose hardness of the sensor is≥30 krad(Si).Furthermore,we propose the first survey results of a magnetometer equipped aboard a Chinese FY-3E satellite in a Sunsynchronous orbit.The data revealed that the AC vector magnetometer can detect transient physical signals such as quasistatic field-aligned currents(~50 nT)and waves at the auroral latitudes.These features render the proposed AC vector magnetometer suitable for space-based applications,particularly those involving the study of geomagnetic activity. 展开更多
关键词 AC vector magnetometer low-resource magneto-impedance sensor fy-3e satellite
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