月球轨道器模块化综合电子设计与实现

以嫦娥五号轨道器为背景,介绍了可重构模块化综合电子方案的设计。从综合电子功能需求分析入手、结合轨道器构型,搭建了综合电子系统体系架构。运用模块化的思路,规划了轨道器综合电子的基本功能模块类型,介绍了内总线的通用化设计,给出了单机的具体配置,并在此基础上进行了综合电子信息流设计。在计算机技术方面,重点介绍了既可以工作于热备份模式,又可以工作于冷备份模式的可重构设计。     

Effect of microgravity on primordial germ cells (PGCs) in silk chicken offspring (Gallus gallus domesticus)

Primordial germ cells (PGCs), precursors of germline cells, display a variety of antigens during their migration to target gonads. Here, we used silk chicken offspring (Gallus gallus domesticus) embryos subjected to space microgravity to investigate the influence of microgravity on PGCs. The ShenZhou-3 unmanned spaceship carried nine fertilized silk chicken eggs, named the flight group, returned to Earth after 7 days space flight. And the control group has the same clan with the flight group. PGCs from flight and control group silk chicken offspring embryos were examined during migration by using two antibodies (2C9 and anti-SSEA-1), in combination with the horseradish peroxidase detection system, and using periodic acid-Schiff’s solution (PAS) reaction. After incubation for about 30 h, SSEA-1 and 2C9 positive cells were detected in the germinal crescent of flight and control group silk chicken offspring embryos. After incubation of eggs for 2–2.5 days, SSEA-1 and 2C9 positive cells were detected in embryonic blood vessels of flight and control group silk chicken offspring embryos. After incubation of eggs for 5.5 days, PGCs in the dorsal mesentery and gonad could also be identified in flight and control group silk chicken offspring embryos by using SSEA-1 and 2C9 antibodies. Based on location and PAS staining, these cells were identified as PGCs. Meanwhile, at the stage of PGCs migration and then becoming established in the germinal ridges, no difference in SSEA-1 or 2C9 staining was detected between female and male PGCs in flight and control group silk chicken offspring embryos. Although there were differences in the profiles of PGC concentration between male and female embryos during the special circulating stage, changing profile of PGCs concentration was similar in same sex between flight and control group offspring embryos. We concluded that there is little effect on PGCs in offspring embryos of microgravity-treated chicken and that PGC development appears to be normal.     

嫦娥五号平动点拓展任务轨道方案研究

中国嫦娥五号探测器成功实现月球采样返回任务,为最大限度利用任务资源,研究了利用嫦娥五号轨道器的平动点拓展任务轨道方案,设计了平动点轨道及其转移轨道.首先,给出了任务轨道设计的轨道动力学模型,包括圆型限制性三体问题模型和精确力模型.其次,基于嫦娥二号和嫦娥5T1平动点拓展任务设计经验,介绍了平动点轨道直接转移与入轨等轨道...     

双极值模糊软K-代数

引入双极值模糊软K-代数的概念,讨论关于双极值模糊软集的交,并运算的相关性质以及它在模糊软K-同态下像的性质。通过双极值模糊集的（t,s）-水平截集给出了双极值模糊软K-代数的等价刻画。     

基于NURBS曲面的雷达散射截面物理光学算法研究

文章实现了一种使用物理光学（PO）计算雷达散射截面的算法。目标模型用非均匀有理B样条（NURBS）曲面建立，并使用等参数等弦长方法剖分为Ⅳ个四边形面元。在剖分面元上，使用Gordon方法将物理光学积分转化为闭合区域线积分。整个算法在保持计算精度的前提下有较高的计算速度。     

基于模块化分工的产业集群升级——以常州邹区灯具产业集群为例

初具规模的常州邹区灯具产业集群存在着和其他产业集群共通的问题,制约着产业的进一步发展.模块化生产分工方式有利于解决邹区产业集群面临的困难.文章结合邹区灯具产业实态,运用模块化分工生产理论,对邹区灯具产业集群升级问题展开研究,提出促进灯具配件企业成为灯具产业链的专业模块供应企业,培育现有中型灯具企业上规模,吸引国内外灯具企业加入邹区产业集群,加快灯具产业集群园区建设,强化新产品开发、打造自主品牌等对策建议.     

Mechanical properties study of particles reinforced aluminum matrix composites by micro-indentation experiments

By using instrumental micro-indentation technique, the microhardness and Young's modulus of SiC particles reinforced aluminum matrix composites were investigated with microcompression-tester(MCT). The micro-indentation experiments were performed with different maximum loads, and with three loading speeds of 2.231, 4.462 and 19.368 mN/s respectively. During the investigation, matrix, particle and interface were tested by micro-indentation experiments. The results exhibit that the variations of Young's modulus and microhardness at particle, matrix and interface were highly dependent on the loading conditions(maximum load and loading speed) and the locations of indentation. Micro-indentation hardness experiments of matrix show the indentation size effects, i.e. the indentation hardness decreased with the indentation depth increasing. During the analysis, the effect of loading conditions on Young's modulus and microhardness were explained. Besides, the elastic–plastic properties of matrix were analyzed. The validity of calculated results was identified by finite element simulation. And the simulation results had been preliminarily analyzed from statistical aspect.     

The relationship between TEC and Earth’s magnetic field during quiet and disturbed days over Istanbul,Turkey

In this study, the impact of Earth’s magnetic field on total electron content (TEC) was studied by using statistical multiple linear regression model and co-integration method. TEC values were measured over the Turkey-Istanbul (ista) station using date of global positioning system (GPS), and the magnetic field components of the Earth were measured from Boğaziçi University, Kandilli Observatory and Earthquake Research Institute, Geomagnetic observatory Istanbul (ISK) station. This examination has been carried out during the dates of March 14–19, 2015 covering the dates of March 17–18, 2015 known in the literature as St. Patrick's Day geomagnetic storm. The three days before the storm (March 14–16) were named as quiet days, whereas the other days (March 17–19) were named as disturbed days after which the two periods were examined separately. It was observed as a result of the examination that the x-component (south-north direction) of the magnetic field had a negative impact on TEC on quiet days, whereas the impact was positive on disturbed days. However, the y-component (east–west direction) of the magnetic field had an inverse relationship of the x-component on the quiet and disturbed days. In addition, it was deduced that the impact coefficient of the x and y-component of the magnetic field was higher on disturbed days in comparison with those on quiet days. The correlation coefficient between the TEC and the components of the Earth’s magnetic field was 0.11 on quiet days and 0.95 on disturbed days. Therefore, it can be stated that the relationship of the TEC values with the geomagnetic field are higher on disturbed days.     

随机恒速运动目标的搜索方程及持续探测概率

根据目标位置的初始分布和速度分布,给出了随机恒速运动目标在任意时刻位置和速度分布密度函数。定义了探测函数、目标存在和探测不成功的联合概率密度函数和目标存活概率函数,建立了基于目标速度分布的搜索方程并给出了其特征迹线解。在目标初始分布和速度分布均为圆正态分布条件下,分析了搜索方程特征迹线的基本特征和持续探测发现概率积分域的形态。给出了一个以直升机吊放声纳探测潜艇为背景的持续探测发现概率的算例,算例表明,对随机恒速运动目标持续探测的发现概率,与对静止目标进行持续探测的发现概率相似,服从时间的指数规律。