越南卫星现状及未来发展

卫星具有覆盖范围广、可长时间稳定运行、无国界限制、安全性高等独特优势,是提升部队作战效能的＂倍增器＂,也是解决大范围战场信息支撑能力问题的有效手段和最佳途径。21世纪初,高速增长的经济推动越南航天事业驶入了发展的快车道,不仅实现了卫星发射的零突破,还相继发射了多颗通信卫星、遥感卫星和试验型纳卫星。文章主要对越南当前的卫星现状进行总结归纳,并分析其未来的发展计划。     

Influence of Al2O3 particles on the microstructure and mechanical properties of copper surface composites fabricated by friction stir processing

The influence of three factors, such as volume percentage of reinforcement particles (i.e. Al₂O₃), tool tilt angle and concave angle of shoulder, on the mechanical properties of Cu–Al₂O₃ surface composites fabricated via friction stir processing was studied. Taguchi method was used to optimize these factors for maximizing the mechanical properties of surface composites. The fabricated surface composites were examined by optical microscope for dispersion of reinforcement particles. It was found that Al₂O₃ particles are uniformly dispersed in the stir zone. The tensile properties of the surface composites increased with the increase in the volume percentage of the Al₂O₃ reinforcement particles. This is due to the addition of the reinforcement particles which increases the temperature of recrystallization by pinning the grain boundaries of the copper matrix and blocking the movement of the dislocations. The observed mechanical properties are correlated with microstructure and fracture features.     

归零制度在学位论文质量保障体系建设中的应用

学位论文是衡量研究生培养质量的重要标志之一。鉴于开题、答辩等重要论文质量监控环节出现的走过场、走形式现象,提出将问题归零制度引入学位论文质量保障体系之中。通过明确归零范围、基本要求、责任主体和处理程序,构建了保障学位论文质量的归零制度设想。     

Return policy: Hassle‐free or your money‐back guarantee?

This article compares the profitability of two pervasively adopted return policies—money‐back guarantee and hassle‐free policies. In our model, a seller sells to consumers with heterogeneous valuations and hassle costs. Products are subject to quality risk, and product misfit can only be observed post‐purchase. While the hassle‐free policy is cost advantageous from the seller's viewpoint, a money‐back guarantee allows the seller to fine‐tune the consumer hassle on returning the product. Thus, when the two return policies lead to the same consumer behaviors, the hassle‐free policy dominates. Conversely, a money‐back guarantee can be more profitable even if on average, high‐valuation consumers experience a lower hassle cost than the low‐valuation ones. The optimal hassle cost can be higher when product quality gets improved; thus, it is not necessarily a perfect proxy or signal of the seller's quality. We further allow the seller to adopt a mixture of these policies, and identify the concrete operating regimes within which these return policies are optimal among more flexible policies. © 2014 Wiley Periodicals, Inc. Naval Research Logistics 61: 403–417, 2014     

数字图像处理的“炮身轴线偏移”检测系统设计与实现

通过解决基于数字图像处理的环境光自适应技术、激光成像自拟合技术、分辨率自适应技术等关键技术,设计并实现"炮身轴线偏移"检测系统,提高了"炮身轴线偏移量"检测效率。经实验验证,该检测系统误差符合检测要求,且具有结构简单、操作简便、精度较高的优点,是可行的。     

TAX EFFICIENCY AND QUALITY/QUANTITY TRADE‐OFFS IN DEFENSE PROCUREMENT*

In this article the effect of defense spending on aggregate output is discussed. Recent publications in this area are reviewed and new additional evidence is provided. The findings presented in this paper are supportive of the positive effect of defense spending. However, in light of the contrary evidence presented in other papers, empirical evidence taken as a whole, suggests that a definitive conclusion about the effect of defense spending at this time should be avoided.     

FPGA的车载防撞雷达系统的设计与实现

根据毫米波汽车防撞雷达的研究现状,讨论了一种基于FPGA为实现核心的总体设计方案,并详细分析该系统硬件结构和软件流程,对处理算法在FPGA上的实现提出相应的优化方法,能有效地提高运算效率的同时降低硬件成本.实验结果表明:该方案对前方车辆相关信息探测迅速准确,运行稳定可靠,能够满足汽车防撞雷达的实时性需求.     

编辑的作者意识与作者的编辑意识

提高期刊出版质量是期刊编辑的共同心愿。进入核心期刊或者按照核心期刊编辑出版刊物,已经成为大多期刊编辑的自觉追求。期刊编辑的作者意识和作者的编辑意识辩证统一,二者良性互动,共同促进期刊编辑出版质量不断提高。     

科学发展观指导大学生思想政治教育质量提升研究

科学发展观不仅为大学生思想政治教育提出了新的理论指导,同时也为其提出了新的更高要求和新的思想方法。加强和改进大学生思想政治教育是事关中华民族前途命运的根本问题,要提升大学生的思想政治教育质量,必须坚持以科学发展观为指导,用科学发展观统领高校思想政治教育,理清工作思路,创新工作模式,促进大学生思想政治素质、科学文化素质和身体素质的全面发展。     

气象探空火箭气温测量不确定度评估方法

在气象火箭测温修正模型基础上,通过误差分析理论,对温度修正及其不确定度评估方法进行研究。根据火箭探空仪在空中下落过程中大气密度变化规律,建立温度修正数学模型,推导得到温度修正公式。根据误差理论,分析影响温度修正的八项误差因素,并逐项给出温度修正误差表达式。以气象火箭实测数据为例,运用上述公式,对探空火箭温度反演不确定度进行分析计算。结果表明:温度反演不确定度在50~60 km较大,最大为3.6 K;40~50 km不确定度为0.3~0.9 K;40 km以下,不大于0.3 K。影响温度不确定度的因素主要是气动加热修正项、滞后效应修正项、结构热传导修正项和传感器对环境热辐射修正项。数据处理时采用参考大气或标准大气仅进行一次修正是不够的,需进行迭代修正,单次修正结果与迭代修正结果差异最大可达5.6 K。