α-混合序列生成的平稳线性过程矩完全收敛性的精确渐近性

利用α-混合序列的矩不等式及α-混合序列生成的平稳线性过程部分和的渐近分布,得到α-混合序列生成的平稳线性过程部分和的矩完全收敛性的精确渐近性.     

一致变化尾的随机和局部精确大偏差

基于带O正则变化独立同分布随机变量的部分和的局部精确大偏差的相关结论,将其对应的随机和分为3个部分,利用次指数函数的相互关系以及控制收敛定理,分别证明每个部分的渐近性.最后证明了在随机变量的密度函数是一致变化尾时,其随机和的局部精确大偏差的渐近性.     

THE PRECISE AND NEW ANALYSIS FOR A MODE Ⅲ GROWING CRACK IN AN ELASTIC-PERFECTLY PLASTIC SOLID

The near crack line field analysis method has been used to investigate into ModeⅢ quasistatically propagating crack in an elastic-perfectly plastic material.Thesignificance of this paper is that the usual small scale yielding theory has been brokenthrough.By obtaining the general solutions of the stresses and the displacement rate ofthe near crack line plastic region,and by matching the general solutions with theprecise elastic fields(not the usual elastic K-dominant fields)at the elastic-plasticboundary,the precise and new solutions of the stress and deformation fields,the sizeof the plastic region and the unit normal vector of the elastic-plastic boundary havebeen obtained near the crack line.The solutions of this paper are sufficiently precisenear the crack line region because the roughly qualitative assumptions of the smallscale yielding theory have not been used and no other roughly qualitative assumptionshave been taken,either.The analysis of this paper shows that the assumingly“steady-state cas     

求解二点边值问题打靶法的一种改进方法

本文讨论两点边值问题的数值解法,利用最小二乘法修正打靶法所需初始参数,将边值问题转化为相应的初值问题与左梯度控制方程合并,引入精细积分法进行求解。通过数值算例表明,该方法是一种求解两点边值问题的有效方法。     

The distribution of the specific pressure in rolling strips

The principle of the distribution of the specific pressure in rolling strips is used not only for calculating the total rolling pressure but also for providing the basis in calculating the widening and in designing the rational roll profile. Hitherto, the results of analysis on this subject in the references are expressed as a function of one dimension, and they cannot reflect the variation of the specific pressure along the width of the contact surface. This paper deals with the two-dimensional expression of the principle of the distribution of the specific pressure with the help of the calculus of variations.     

基于递推最小二乘平方差的GPS精密单点定位精度研究

对传统GPS单点定位、差分GPS定位和GPS精密单点定位进行了比较。建立了GPS精密单点定位无电离层组合的数学模型。建立了递推最小二乘平差进行参数估算的数学模型,并利用该方法进行相位平滑伪距处理。分析了该方法对伪距观测误差的影响。利用bernese软件和据此编制的程序,并利用IGS跟踪站的观测数据进行了接收机三维坐标的解算。将IGS观测值坐标作为真值,解算值和真值之间的偏差作为定位误差。仿真结果表明,经过递推最小二乘伪距平滑处理后,精密单点定位的误差在北方向、东方向、高度方向上都小于0.02 m。     

新医改背景下公立医院运营成本精准管控体系构建

目的：针对公立医院运营成本在管理和控制过程中受到经济全球化的影响,存在效率和精准度低的问题,为此提出了新医改背景下公立医院运营成本精准管控体系构建研究。方法：在新医改背景下,通过公立医院运行成本信息,健全了公立医院运营成本管控的组织结构,并对公立医院运营成本管控组织结构进行了优化,结合公立医院运营成本管控规范的优化设计,优化了公立医院运营成本精准管控策略,基于公立医院生产的标准成本和资源的标准消耗量的计算,制定了公立医院运营成本标准。结果：通过消除外部经营环境的影响,优化调整了公立医院生产的标准成本和资源的标准消耗量,制定了公立医院产品标准成本,最后通过完善公立医院运营成本的组织结构,实现了公立医院运营成本精准管控体系的构建。结论：实验结果表明,新医改背景下公立医院运营成本精准管控体系在管控效率和精准度方面,都具有更好的管控性能。     

精细指数积分法在卫星编队飞行动力学中的应用

编队飞行卫星间的距离远小于卫星的轨道半径, 其动力学方程表现为弱非线性。针对弱非线性方程的求解, 提出精细指数积分方法, 用精细积分法求解指数积分方法中的指数矩阵。用精细指数积分法和Runge-Kutta方法, 在不同条件下求解弱非线性方程的算例, 验证了精细指数积分法的有效性。通过Lagrange方程, 建立卫星编队飞行动力学方程的半线性形式, 用精细指数积分方法与Runge-Kutta方法求解方程。数值计算结果表明, 与同阶的Runge-Kutta求解弱非线性微分方程相比, 精细指数积分法具有更高的精度, 为卫星编队飞行动力学仿真提供了一种有效的数值算法。     

区间分析法在精细注水管柱设计方面的应用

随着油田开发进入中后期,油层及夹层的厚度越来越小,传统的大卡距大间距分层注水工艺管柱设计已经不 能满足要求,为了提高采油效率,小卡距的精细分层注水工艺应运而生,然而此工艺具有卡封层数多和单层卡距小的 特点,这对管柱力学量的精确计算提出了更高的要求。针对此问题,提出了一种区间分析法,考虑了管柱变形量的主 要不确定因素,建立了三维不确定性管柱力学模型并得到了管柱变形量区间,最后结合现场数据对分析结果进行了验 证,结果表明：现场数据与设计数据高度吻合,提高了注水合格率,对精细注水管柱的设计具有一定的指导意义。     

Precise orbit determination of a maneuvered GEO satellite using CAPS ranging data

Wheel-off-loadings and orbital maneuvers of the GEO satellite result in additional accelerations to the satellite itself. Complex and difficult to model, these time varying accelerations are an important error source of precise orbit determination (POD). In most POD practices, only non-maneuver orbital arcs are treated. However, for some applications such as satellite navigation RDSS services, uninterrupted orbital ephemeris is demanded, requiring the development of POD strategies to be processed both during and after an orbital maneuver. We in this paper study the POD for a maneuvered GEO satellite, using high precision and high sampling rate ranging data obtained with Chinese Area Positioning System (CAPS). The strategy of long arc POD including maneuver arcs is studied by using telemetry data to model the maneuver thrust process. Combining the thrust and other orbital perturbations, a long arc of 6 days’ CAPS ranging data is analyzed. If the telemetry data are not available or contain significant errors, attempts are made to estimate thrusting parameters using CAPS ranging data in the POD as an alternative to properly account for the maneuver. Two strategies achieve reasonably good data fitting level in the tested arc with the maximal position difference being about 20 m. Supported by the National Natural Science Foundation of China (Grant No. 10703011) and the Science & Technology Commission of Shanghai Municipality of China (Grant No. 06DZ22101)