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61.
By use of GMS-4 infrared brightness temperature and visible albedo data from January toFebruary in 1995,the method for extracting of sea ice parameters is developed.The digital remotesensing picture is obtained on Liaodong Bay.Based on the difference in physical properties betweenice and water,a criterion distinguishing ice from water is set up.Ice thickness has been calculatedaccording to the relationship between ice thickness and brightness as well as albedo.Iceconcentration is retrieved due to the difference on albedo between ice and water.The resultsindicate that the accuracy of ice-water distinguishing is 84.8%,the errors of ice thickness and iceconcentration are 3.8 cm and 22%,respectively. 相似文献
62.
为进一步提高观测频次和信噪比,近年来各国新一代静止气象卫星均采用三轴稳定工作模式对地扫描成像。为了精确提取遥感目标物所在地点关于地表、云和大气状态的定量参数产品,必须要解决图像配准和定位问题。轨道漂移运动引起卫星视轴在地球表面上移动,导致连续图像之间产生相对位移,影响云图动画的图像配准精度。以2016年12月发射的中国风云四号卫星成像仪为研究对象,给出了图像参考基准的严密定义,研究了一种轨道运动补偿OMC(Orbit Motion Compensation)方法。通过给成像仪2维扫描机构增加转角补偿的方法在卫星上实时引导视线扫描路径,卫星相当于在理想轨道位置的视角成像。得到的遥感图像均被配准到地球固定网格FG(Fixed Grid),保持相对固定的几何定位关系。由于这种在卫星上完成的补偿剥离了L0级图像数据与卫星轨道测量信息之间的关系,从根源上保证了原始图像的长周期定位稳定性。为证明方法的正确性,利用风云四号卫星在轨测试的遥感图像L0级数据进行了试验验证。结果表明,云图动画中南北方向相对运动距离由973.0μrad缩小至75.6μrad,东西方向由205.8μrad缩小至81.2μrad。星上轨道运动补偿有效削弱了周期性轨道运动对图像定位与配准的干扰,显著提升图像配准精度。针对未来带有长线阵的新型静止卫星成像仪发展趋势,分析了进行星上轨道运动补偿时引起的长线阵探测器边缘像元误差问题,提出了采用电推进系统对卫星轨道倾角进行高精度保持控制来降低边缘误差的解决方案。 相似文献
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66.
By use of GMS-4 infrared brightness temperature and visible albedo data from January to February in 1995,the method for extracting of sea ice parameters is developed.The digital remote sensing picture is obtained on Liaodong Bay.Based on the difference in physical properties between ice and water,a criterion distinguishing ice from water is set up.Ice thickness has been calculated according to the relationship between ice thickness and brightness as well as albedo.Ice concentration is retrieved due to the difference on albedo between ice and water.The results indicate that the accuracy of ice-water distinguishing is 84.8%,the errors of ice thickness and ice concentration are 3.8 cm and 22%,respectively. 相似文献
67.
现有的极轨微波仪器有着较强的穿云能力,空间分辨率较低,故目前而言,国内外鲜有针对微波探测器的视差分析研究,但若未来在静止轨道上搭载空间分辨率较高的静止轨道微波探测器,则微波视场内的视差问题不容忽视。针对未来发展的静止轨道卫星微波探测器,利用辐射传输模式CRTM模拟该类仪器的亮温,并分析其受视场内云影响所产生的视场偏差,结果表明空间分辨率越高,视差问题越明显;天顶角越大,云顶高度越高,视差越大。除此之外,以台风和高云的个例对实际情况中微波探测仪内视差误差进行了展示,说明静止轨道微波仪器尽管有较高的时间分辨率,但是因为视差的存在,仍然会对台风预警的准确性产生影响。 相似文献
68.
地表参数定量遥感反演是遥感科学研究的重要环节.21世纪以来,地球静止气象卫星数据在地表参数遥感反演中受到越来越多的重视.本文对利用地球静止气象卫星进行地表参数遥感反演研究的进展进行了综述.文章首先简单介绍了当前正在运行的欧盟Meteosat、美国GOES-R、日本葵花和中国风云静止卫星系统,随后详细总结了不同卫星系统估... 相似文献
69.
Based on Multifunctional Transport Satellite data and the infrared window-texture detection algorithm, the level of overshooting top(OT) activity within a tropical cyclone(TC), which is defined as the hourly mean number of OT occurrence,was statistically investigated in the western North Pacific basin for the period 2005–12. Based on the level of OT activity,the samples were divided into OT and non-OT cases or high-activity-OT(HA-OT) and low-activity-OT(LA-OT) cases. The differences in large-scale environmental variables between OT(HA-OT) and non-OT(LA-OT) cases were examined 12 hours prior to the OT occurrence. Statistical analysis showed that environmental differences did exist between the OT and non-OT cases. The OTs were more skewed towards the early stage of the TC life cycle, and mostly concentrated in low latitudes.Meanwhile, a sufficiently deep warm-water layer, large temperature difference between the upper- and lower-level troposphere, large humidity at the middle and upper levels, and large atmospheric instability, were favorable for OT occurrence.The differences in large-scale environmental characteristics between HA-OTs and LA-OTs were not as significant as those between OTs and non-OTs, but the HA-OT samples tended to occur when the vertical shear was weak and the TC intensity was low. Finally, statistical models were designed to predict the OT and HA-OT. When at least three OT(HA-OT) predictor thresholds were satisfied, the Peirce skill score reached a maximum value of 0.49(0.30). 相似文献
70.
CEI对静止轨道共位卫星的轨道确定 总被引:1,自引:0,他引:1
主要考察了CEI对静止轨道共位卫星的轨道确定能力。仿真结果表明,利用CEI对共位卫星进行定轨时,需采用基线阵列。对于110°E共位卫星采用三亚-昆明基线阵列、10 km基线和2 d的数据,可使绝对轨道精度达百米级;外推至14 d时,相对轨道精度保持在m级。同样,要使绝对和相对轨道精度达到相同的量级,对于80°E共位卫星,需选用昆明-三亚基线阵列、100 km基线和1 d的观测弧段;对于140°E共位卫星,需选用上海-三亚基线阵列5、0 km基线和2 d的观测弧段。 相似文献