Efficient and rapid accuracy estimation of the Earth’s gravitational field from next-generation GOCE Follow-On by the analytical method

Firstly, a new analytical error model of the cumulative geoid height using the three-dimensional diagonal tensors of satellite gravity gradiometry (SGG) is introduced based on the variance-covariance matrix principle. Secondly, a study for the requirements demonstration on the next-generation GOCE Follow-On satellite gravity gradiometry system is developed using different satellite orbital altitudes and measurement accuracies of satellite gravity gradiometer by the new analytical error model of SGG. The research results show that it is preferable to design satellite orbital altitudes of 300 km-400km and choose the measurement accuracies of 10-13/s2 -10-15/s2 from satellite gravity gradiometer. Finally, the complementarity of the four-stage satellite gravity missions, including past CHAMP, current GRACE, and GOCE, and next-generation GOCE Follow-On, is contrastively demonstrated for precisely recovering the Earth’s full-frequency gravitational field with high spatial resolution.     

气相输运沉积制备c轴择优取向的碘化铋薄膜

铋基卤化物材料因其无毒和优良的光电性能而显示出巨大的应用潜力。BiI₃作为一种层状重金属半导体,已被用于X射线检测、γ射线检测和压力传感器等领域,最近其作为一种薄膜太阳能电池吸收材料备受关注。本文采用简单的气相输运沉积(VTD)法,以BiI₃晶体粉末作为蒸发源,在玻璃基底上得到高质量c轴择优取向的BiI₃薄膜。并通过研究蒸发源温度和沉积距离对薄膜物相和形貌的影响,分析了BiI₃薄膜择优生长的机理。结果表明VTD法制备的BiI₃薄膜属于三斜晶系,其光学带隙为~1.8 eV。沉积温度对薄膜的择优取向有较大影响,在沉积温度低于270 ℃时,沉积的薄膜具有沿c轴择优取向生长的特点,超过此温度,c轴择优取向生长消失。在衬底温度为250 ℃、沉积距离为15 cm时制备的薄膜结晶性能最好,晶体形貌为片状八面体。     

ZnO-PSAⅡ型异质结界面电荷转移过程研究

采用稳态光致发光光谱和纳秒时间分辨瞬态光谱(NTRT-PL)表征,揭示ZnO-PSA II型纳米异质结光生载流子电荷转移过程,通过甲基橙光降解实验,测得ZnO-NRs和ZnO-PSA紫外光降解率分别为25.5;和60.1;,光降解率提高到2.4倍,表明II型异质结相对于单一半导体而言,能促进光生载流子在界面间电荷转移,有利于载流子的分离.     

“反尖端”界面不稳定性数值计算分析

利用可压缩多介质黏性流动和湍流大涡模拟代码(MVFT),在超算平台上对"反尖端"界面不稳定性及其诱发的湍流混合问题进行了大规模三维数值模拟分析。数值模拟结果清晰地显示了冲击波加载界面后分解产生的冲击波、稀疏波、压缩波及其在SF6气体中的运动和相互作用,以及波多次加载界面的复杂过程,波和界面的每一次作用都会加速湍流混合区的发展和物质混合。"反尖端"界面受冲击波加载后发生反相而形成典型的大尺度壁面气泡和中心轴尖钉结构,该大尺度结构基本确定了湍流混合区的平均几何特征和包络范围而不依赖计算网格。高分辨率的计算网格下,捕捉到了更精细的小尺度湍涡结构和更强的湍流脉动,显示了湍流混合区所具有的复杂结构和特征。     

地球重力场空间探测: 回顾与展望

地球重力场的科学数据在地球测绘学、冰川学、陆地水循环、固体地球物理、灾害监控及国防军事等领域具有重要应用价值. 美、德合作研制的地球重力场反演与气候实验(gravity recovery and climate experiment, GRACE)卫星, 有力地推动了地球重力场测量、反演和应用. 为进一步提高重力卫星科学数据的时、空分辨率, 扩展应用领域, 中国及欧美等国都考虑发射升级的重力卫星, 即后GRACE 计划(GRACE-follow-on). 本文将简单回顾重力卫星的发展历程, 介绍重力卫星的数据采集技术和反演方法, 亦着重阐述后GRACE计划的测量方法学、关键技术及预期结果.      

A contrastive study on the influences of radial and three-dimensional satellite gravity gradiometry on the accuracy of the Earth's gravitational field recovery

The accuracy of the Earth’s gravitational field measured from the gravity field and steady-state ocean circulation explorer(GOCE),up to 250 degrees,influenced by the radial gravity gradient V zz and three-dimensional gravity gradient V ij from the satellite gravity gradiometry(SGG) are contrastively demonstrated based on the analytical error model and numerical simulation,respectively.Firstly,the new analytical error model of the cumulative geoid height,influenced by the radial gravity gradient V zz and three-dimensional gravity gradient V ij are established,respectively.In 250 degrees,the GOCE cumulative geoid height error measured by the radial gravity gradient V zz is about 2 1/2 times higher than that measured by the three-dimensional gravity gradient V ij.Secondly,the Earth’s gravitational field from GOCE completely up to 250 degrees is recovered using the radial gravity gradient V zz and three-dimensional gravity gradient V ij by numerical simulation,respectively.The study results show that when the measurement error of the gravity gradient is 3×10 12 /s 2,the cumulative geoid height errors using the radial gravity gradient V zz and three-dimensional gravity gradient V ij are 12.319 cm and 9.295 cm at 250 degrees,respectively.The accuracy of the cumulative geoid height using the three-dimensional gravity gradient V ij is improved by 30%-40% on average compared with that using the radial gravity gradient V zz in 250 degrees.Finally,by mutual verification of the analytical error model and numerical simulation,the orders of magnitude from the accuracies of the Earth’s gravitational field recovery make no substantial differences based on the radial and three-dimensional gravity gradients,respectively.Therefore,it is feasible to develop in advance a radial cold-atom interferometric gradiometer with a measurement accuracy of 10 13 /s 2-10 15 /s 2 for precisely producing the next-generation GOCE Follow-On Earth gravity field model with a high spatial resolution.     

爆轰驱动铝飞层扰动增长的数值模拟（英文）

建立了研究炸药爆轰驱动条件下金属材料Rayleigh-Taylor不稳定性问题的实验技术和数值模拟方法。利用该实验技术和数值模拟方法研究了炸药爆轰驱动条件下,铝飞层界面Rayleigh-Taylor不稳定性增长规律,数值模拟显示界面扰动振幅以指数规律增长。数值模拟结果和实验定性相符,但是定量相比有较大差别,原因是高压高应变率加载条件下铝的强度增强,而数值模拟时所采用的SG本构模型在这样的加载条件下低估了铝的强度而导致对扰动增长致稳作用不足。然后在数值模拟中,通过改变材料的初始剪切模量和初始屈服强度,发现在一定范围内,初始剪切模量对材料动态屈服强度没有影响,而初始屈服强度增大可以明显提高材料的动态屈服强度,达到抑制扰动增长的目的,表明材料屈服强度主导界面扰动增长。     

Physical analysis on improving the recovery accuracy of the Earth’s gravity field by a combination of satellite observations in along-track and cross-track directions

The physical investigations on the accuracy improvement to the measurement of the Earth＇s gravity field recovery are carried out based on the next-generation Pendulum-A/B out-of-plane twin-satellite formation in this paper. Firstly, the Earth＇s gravity field complete up to degree and order 100 is, respectively, recovered by the collinear and pendulum satellite formations using the orbital parameters of the satellite and the matching accuracies of key payloads from the twin GRACE satellites. The research results show that the accuracy of the Earth＇s gravity field model from the Pendulum-A/B satellite formation is about two times higher than from the collinear satellite formation, and the further improvement of the determination accuracy of the Earth＇s gravity field model is feasible by the next-generation Pendulum-A/B out-of-plane twin-satellite formation. Secondly, the Earth＇s gravity field from Pendulum-A/B complete up to degree and order 100 is accurately recovered based on the orbital parameters of the satellite （e.g., an orbital altitude of 400 km, an intersatellite range of 100 km, an orbital inclination of 89° and an orbital eccentricity of 0.001）, the matching accuracies of space- borne instruments （e.g. 10-6 m in the intersatellite range, 10-3 m in the orbital position, 10-6 m/s in orbital velocity, and 10-11 m/s2 in non-conservative force）, an observation time of 30 days and a sampling interval of 10 s. The measurement accuracy of the Earth＇s gravity field from the next-generation Pendulum-A/B out-of-plane twin-satellite formation is full of promise for being improved by about l0 times compared with that from the current GRACE satellite formation. Finally, the physical requirements for the next-generation Pendulum-A/B out-of-plane twin-satellite formation are analyzed, and it is proposed that the satellite orbital altitude be preferably designed to be close to 400±50 km and the matching precision of key sensors from the Pendulum-A/B mission be about one order of magnitude higher tha     

线型扩散性分布不均对螺旋波影响的浅析

以LuoRudy91模型为基础,研究了线型扩散性分布不均匀对心脏中的螺旋波的影响。结果表明：线形式的扩散性分布不均匀对螺旋波有着重要影响,甚至可能导致它们的湮灭。     

金属锡Rayleigh-Taylor不稳定性对模型参数敏感性的数值分析

利用自研的爆轰与冲击动力学欧拉计算程序和Steinberg-Guinan(SG)本构模型,数值模拟分析了样品初始参数(初始振幅、初始波长、样品初始厚度)和SG本构模型初始参数对爆轰驱动锡Rayleigh-Taylor(RT)不稳定性增长的影响。结果表明金属锡样品的初始参数对其RT不稳定性增长有很大的影响。RT不稳定性增长随着初始振幅的减小而减小,且存在一个截止初始振幅;存在一个最不稳定的模态(波长),当初始波长大于该波长时,RT不稳定性增长随着初始波长的减小而增大,反之,RT不稳定性增长随着初始波长的减小而减小;样品厚度的增大可以抑制RT不稳定性增长,而且存在一个样品截止厚度。金属锡的RT不稳定性增长对其SG本构模型应变硬化系数和应变硬化指数的变化不敏感,而对压力硬化系数和热软化系数比较敏感。从采用扰动增长法预估材料强度的角度来说,修正压力硬化系数以获得锡合理的材料强度是合理的途径。