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宽波段光谱的小行星表面温度反演方法
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作者 陈丰熠 张玉贵 +1 位作者 王伟刚 徐彭梅 《光谱学与光谱分析》 SCIE EI CAS CSCD 北大核心 2023年第4期1162-1167,共6页
小行星表面温度是研究行星热物理特性的关键参数。太阳系中小天体的轨道动力学研究具有多种实际应用,包括预测行星体轨道和撞击产生的陨石坑率、选择航天器合适的探测采样目标。对于近地天体,分析它们的轨道结构、星体的轨道演化和未来... 小行星表面温度是研究行星热物理特性的关键参数。太阳系中小天体的轨道动力学研究具有多种实际应用,包括预测行星体轨道和撞击产生的陨石坑率、选择航天器合适的探测采样目标。对于近地天体,分析它们的轨道结构、星体的轨道演化和未来的偏移轨迹等近地天体动力学特性具有重要意义。中国即将发射“天问二号”,对近地小行星2016HO3进行热辐射探测和风化层采样。“天问二号”预计在不远的将来到达环绕2016HO3的轨道。研究了一种温度-比辐射率分离算法,用于从“欧西里斯-雷克斯”热辐射光谱仪(OTES)辐亮度数据中,计算与小行星2016HO3热物理性质相近的行星“贝努”(Bennu)的表面温度。温度-比辐射率分离算法融合了发射率归一化法(NEM)、比值法(RAT)、发射率最大最小值差法(MMD),是目前精度较高的一种表面温度反演算法。为了验证算法的准确性,使用了CRISM光谱库的光谱数据,通过改变目标的温度和算法使用波段,来研究算法对二者的敏感性。其中,因为仪器波段限制等原因,尚无使用波段对算法的误差推导。研究结果表明:(1)设置温度范围为115~415 K,步长5 K,随着温度的增加,反演温度的均方根误差增加,而发射率的误差大致不变。(2)样本温度为295 K,算法使用的波段起点为7.5μm,采样间隔0.04μm,终点为10~13.8μm,步长0.2μm。发现波长范围在7.5~13.8μm,算法的MMD模块的精度最高。使用算法求解行星“贝努”的表面温度,结果表明:在剔除了大太阳高度角和高纬像素的情况下,算法计算的温度的误差平均值为-0.3660 K,误差的标准差为1.0393 K。 展开更多
关键词 温度比辐射率分离算法 Bennu(贝努) 2016HO3 行星表面温度反演
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A Method to Determine the Mean Temperature at the Planet Surface
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作者 GAOChong-Yi 《Communications in Theoretical Physics》 SCIE CAS CSCD 2003年第2X期241-243,共3页
The escape time of a given species of partlcles in the planetary atmosphere is related to atmospheric temperature. The mean temperature at the planet surface may be inferred from the escape of a given kind of particle... The escape time of a given species of partlcles in the planetary atmosphere is related to atmospheric temperature. The mean temperature at the planet surface may be inferred from the escape of a given kind of particles in the planetary atmosphere. For example, CH4 escaping from the Pluto atmosphere results in the variation of its partial pressure and escape time, then the mean temperature at the Pluto surface, 42.2 K, is got on the barns of it. 展开更多
关键词 行星温度 行星表面 行星大气 逃逸时间 冥王星
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人类活动对气候的影响
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作者 裘建强 《环境科学动态》 1981年第6期8-9,共2页
要进一步了解人类活动对气候状况的影响,现代气候稳定性问题非常重要。目前的气候状况只代表长期气候演变中的短暂一瞬,长期气候演变是通过对古气候的研究弄清楚的。古气候研究表明。
关键词 古气候研究 气候演变 人类活动 气候状况 现代气候 行星温度 二氧化碳浓度 大气透明度 反照率 海洋环流
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Identifying Global Monsoon Troughs and Global Atmospheric Centers of Action on a Pentad Scale 被引量:18
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作者 QIAN Wei-Hong TANG Shuai-Qi 《Atmospheric and Oceanic Science Letters》 2010年第1期1-6,共6页
Using two datasets of global pentad grid precipitation and global 850 hPa geopotential height during 1979-2007,this study identified global monsoon troughs and global atmospheric centers of action (ACAs) on a pentad s... Using two datasets of global pentad grid precipitation and global 850 hPa geopotential height during 1979-2007,this study identified global monsoon troughs and global atmospheric centers of action (ACAs) on a pentad scale.The global monsoon troughs consist of planetary-scale monsoon troughs and peninsula-scale monsoon troughs.Forced by seasonal variations in solar radiation,the inter-tropical convergence zones (ITCZs) represent the planetary-scale monsoon troughs,which are active and shift over the tropical North Pacific,the tropical North Atlantic,and the tropical South Indian oceans.The peninsula-scale monsoon troughs are originated from regional land-sea topography and varied with contrasts in seasonal land-sea surface temperatures and precipitation.During the boreal summer,five peninsula-scale troughs and one planetary-scale trough are distributed in the Asia-Northwest Pacific (NWP) region.In total,22 troughs,nine monsoon troughs,and 19 ACAs in the lower troposphere were identified.Relevant ACAs may be useful in constructing regional monsoon and circulation indices. 展开更多
关键词 monsoon trough planetary scale peninsula scale atmospheric centers of action pentad scale
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Analysis of residual gas disturbance on the inner satellite of Inner Formation Flying System 被引量:1
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作者 GU ZhenFeng WANG ZhaoKui ZHANG YuLin 《Science China(Technological Sciences)》 SCIE EI CAS 2012年第9期2511-2517,共7页
The Inner Formation Flying System (IFFS) consisting of an freely flying in the shield cavity can construct a pure gravity outer satellite and an inner satellite which is a sphere proof mass orbit to precisely detect... The Inner Formation Flying System (IFFS) consisting of an freely flying in the shield cavity can construct a pure gravity outer satellite and an inner satellite which is a sphere proof mass orbit to precisely detect the earth gravity field. The residual gas in the cavity is a significant disturbance source due to the temperature inhomogeneity and relative motion of the inner satellite. The expressions of the disturbance forces were derived based on the property of rarefied gas, including the radiometer effect and the damping force. According to the current design of IFFS, heat transfer analysis of the cavity and the inner satellite was carried out, and the surface temperature distribution of the cavity and the inner satellite was given. The relative motion of the inner satellite was obtained from the formation control simulation of IFFS. Then the residual gas disturbance was calculated. The disturbance acceleration acting on the inner satellite due to the radiometer effect was on the order of 10^-11 m s^-2 and the damping acceleration was on the order of 10^-15 m s^-2. 展开更多
关键词 Inner Formation Flying System inner satellite residual gas radiometer effect residual gas damping
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