Precise orbit determination for the GRACE mission using only GPS data

The GRACE (gravity recovery and climate experiment) satellites, launched in March 2002, are each equipped with a BlackJack GPS onboard receiver for precise orbit determination and gravity field recovery. Since launch, there have been significant improvements in the background force models used for satellite orbit determination, most notably the model for the geopotential. This has resulted in significant improvements to orbit accuracy for very low altitude satellites. The purpose of this paper is to investigate how well the orbits of the GRACE satellites (about 470 km in altitude) can currently be determined using only GPS data and based on the current models and methods. The orbit accuracy is assessed using a number of tests, which include analysis of orbit fits, orbit overlaps, orbit connecting points, satellite Laser ranging residuals and K-band ranging (KBR) residuals. We show that 1-cm radial orbit accuracy for the GRACE satellites has probably been achieved. These precise GRACE orbits can be used for such purposes as improving gravity recovery from the GRACE KBR data and for atmospheric profiling, and they demonstrate the quality of the background force models being used.     

几何精度因子对GRACE卫星几何轨道精度影响分析

分析了GDOP值与GRACE卫星几何轨道精度之间的关系,发现定轨精度较差的历元其GDOP值普遍较大甚至异常,进一步研究发现GDOP值异常现象是因剔除个别含有粗差的卫星而导致的,进而通过设置GDOP值阈值的方式剔除发生GDOP值异常的历元。实验结果表明,GDOP值阈值设置为50,将大于该阈值的历元剔除,能够有效抑制个别历元精度较差的情况,最终的RMS在地固系X,Y,Z3个方向分别为0.029m,0.043m,0.029m,实现了几何法厘米级精密定轨的目标。     

盐胁迫下梭梭幼苗膜脂过氧化和保护酶活性

使用0、50、100、200、350、500 mmol/L NaCl处理梭梭幼苗,分三次取样,并测其相应指标,结果表明梭梭幼苗细胞膜透性在10天时保持稳定;当胁迫到20天、30天时,同化枝膜透性随盐浓度的增加及胁迫时间的延长逐渐增加.整个试验过程中,丙二醛含量逐渐增加,但前期增加幅度不大,后期梭梭幼苗同化枝的丙二醛含量在NaCl胁迫30天时为2.569 μmol·g-1.SOD和POD活性在整个试验过程中相对于对照而言整体呈增加趋势,但在前期增加得较快,后期较慢.CAT活性在整个过程中则一直呈增加趋势.     

Application of a BEM time stepping algorithm in understanding complex unsteady propulsion hydrodynamic phenomena

We solve the problem of unsteady potential flow around a system of arbitrarily moving rigid or flexible, lifting or non-lifting bodies, in an infinite fluid free of distributed vorticity. For the solution we use a time stepping algorithm and a potential based formulation of the corresponding free BVP. Nonlinear free shear layer dynamics are included in our modeling. This is a major innovation in treating complex unsteady propulsion problems since no simplifying assumptions (like that of a helicoidal wake) are used regarding the wake model. Bilinear quadrilateral elements are used to describe body and shear layer geometry at each time t. Three types of Kutta conditions can be alternatively applied for the determination of the shed vorticity from lifting bodies. The theoretical and numerical aspects of the method are presented followed by a number of applications, elucidating the qualitative and quantitative physical characteristics of a number of complex unsteady propulsion problems.     

96孔酶标板法测定对虾血淋巴的过氧化物酶相对活性的初步研究

过过氧氧化化物物酶酶（（ＰＰＯＯＤＤ））广广泛泛存存在在于于真真核核生生物物体体内内 ,,在在清清除除自自由由基基 ((ＯＯ - - )) ,,防防止止生生物物分分子子损损伤伤方方面面有有十十分分重重要要的的作作用用。。因因此此通通过过测测量量对对虾虾血血淋淋巴巴的的过过氧氧化化物物酶酶活活性性大大小小可可以以推推测测对对虾虾的的生生理理状状态态 ,,甚甚至至可可用用其其辅辅助助检检测测或或诊诊断断对对虾虾病病害害的的生生理理指指标标。。丁丁美美丽丽等等采采用用改改良良的的连连苯苯三三酚酚自自氧化化法法测测定定中…     

Numerical flow analysis of single-stage ducted marine propulsor

The present work has solved 3D incompressible RANS equations on a rotating, non-orthogonal multi-blocked grid to efficiently analyze a ducted marine propulsor with rotor–stator interaction. To handle the interface boundary between a rotor and a stator, the sliding multi-block technique using the cubic spline interpolation and the bilinear interpolation was applied. To validate the present code, the flow of a single stage turbine flow was simulated. Time averaged pressure coefficients were compared with experiments and good agreements were obtained. After the code validation, the flowfield around a single-stage ducted marine propulsor having a single stage of rotor and stator was successfully simulated and the hydrodynamic performance coefficients were computed.     

An Ensemble-Based Three-Dimensional Variational Assimilation Method for Land Data Assimilation

Land surface models are often highly nonlinear with model physics that contain parameterized discontinuities. These model attributes severely limit the application of advanced variational data assimilation methods into land data assimilation. The ensemble Kalman filter （EnKF） has been widely employed for land data assimilation because of its simple conceptual formulation and relative ease of implementation. An updated ensemble-based three-dimensional variational assimilation （En3-DVar） method is proposed for land data assimilation This new method incorporates Monte Carlo sampling strategies into the 3-D variational data assimilation framework. The proper orthogonal decomposition （POD） technique is used to efficiently approximate a forecast ensemble produced by the Monte Carlo method in a 3-D space that uses a set of base vectors that span the ensemble. The data assimilation process is thus significantly simplified. Our assimilation experiments indicate that this new En3-DVar method considerably outperforms the EnKF method by increasing assimilation precision. Furthermore, computational costs for the new En3-DVar method are much lower than for the EnKF method.     

用于控制高柔结构振动的POD技术

本文通过模型试验和理论分析研究了一种控制高柔结构振动的新方法－－－ＰＯＤ（摆、油阻尼器）减振系统。文中详细分析了其减震原理,并提出了与试验结果相吻合的三角形非缄性滞回模型。试验结果表明,在接近调谐状态下ＰＯＤ法可减振４８％。数据计算的结果也表明,ＰＯＤ不仅减振效果比ＴＭＤ高得多,而且有效频带也宽得多。ＰＯＤ系统具有造价低、易安装、占用空间小、免维护等优点,可用于风可于震等荷载引起的电视塔、悬索桥塔     

Influence of Ice Size Parameter Variation on Hydrodynamic Performance of Podded Propulsor

During ice-breaking navigation, a massive amount of crushed ice blocks with different sizes is accumulated under the hull of an ice-going ship. This ice slides into the flow field in the forward side of the podded propulsor, affecting the surrounding flow field and aggravating the non-uniformity of the propeller wake. A pulsating load is formed on the propeller, which affects the hydrodynamic performance of the podded propulsor. To study the changes in the propeller hydrodynamic performance during the ice podded propulsor interaction, the overlapping grid technique is used to simulate the unsteady hydrodynamic performance of the podded propulsor at different propeller rotation angles and different ice block sizes. Hence, the hydrodynamic blade behavior during propeller rotation under the interaction between the ice and podded propulsor is discussed. The unsteady propeller loads and surrounding flow fields obtained for ice blocks with different sizes interacting with the podded propulsor are analyzed in detail. The variation in the hydrodynamic performance during the circular motion of a propeller and the influence of ice size variation on the propeller thrust and torque are determined. The calculation results have certain reference significance for experiment-based research, theoretical calculations and numerical simulation concerning ice podded propulsor interaction.     

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