两种浸入式边界方法的比较

介绍两类不同的浸入式边界方法及其对它的改进. 然后采用均匀矩形交错网格和压力校正投影法,对不可压流场中的二维圆柱绕流进行了数值求解并对比了两类方法的精度.计算分析表明,连续显力法具有构造简单,适用性强的优点. 但离散隐力法在物面边界精度上要优于前者. 改进后,在二阶精度的离散格式下物面边界精度较低的显示力源法的精度有一定提高,同时发现,加密网格以提高数值精度的方法对于连续显力法并不总是有效.而同样格式下,离散隐力法具有更高精度,其中预测-校正离散隐力法可以在此基础上获得更小的计算误差和更快的收敛速度. 数值解与文献已有的数值和实验结果吻合得很好,表明边界算法及其程序是可靠和有效的.      

高精度海洋重力测量中厄特弗斯改正误差分析

为有效减小厄特弗斯改正的误差,提高重力异常测量值的精度,在分析厄特弗斯改正计算模型的基础上,就载体的速度误差、航向误差及纬度误差对厄特弗斯改正误差的影响进行了仿真分析.在误差分析时,首先对厄特弗斯改正模型求取各变量的偏导,从而得到各变量与厄特弗斯修正误差之间的关系,并以此为基础采用三维视图和数字计算相结合的方法给出了具体的分析结果.仿真结果表明,速度误差是厄特弗斯改正误差的最大影响因素.在某一确定测量误差要求下,速度误差的精度要求随载体所处纬度和航向角的变化而变化;在φ:0°,A=90.时,要保证厄特弗斯改正误差小于0.1 mGal,载体速度测量误差需小于0.013m/s.     

Defects in Statically Unstable Solids: The Case for Cubic Perovskite α-CsPbI3

High-temperature phases of solids are often dynamically stable only. First-principles study of point defects in such solids at 0 K is prohibited by their static instability, which results in random structures of the defect-containing supercell so that the total energy of the supercell is randomly affected by structural distortions far away from the defect. Taking cubic perovskite α-Cs Pb I3 as an example, we first present the problem incurred by the static instability and then propose an approac...     

拿破仑与拿破仑三角形

1．拿破仑 说起拿破仑·波拿巴（1769—1821）,人们总记起这位叱咤风云的法国皇帝,然而,他的一生与数学也有着不解之缘却鲜为人知．他出生于科西嘉岛的平民家庭,少年时期,就对数学有浓厚的兴趣,1784年,著名数学家拉普拉斯发现拿破仑有杰出的数学才能,这成为他能够被巴黎军校录取的一个重要原因．     

The dual role of multiple-transistor charge sharing collection in single-event transients

As technologies scale down in size, multiple-transistors being affected by a single ion has become a universal phenomenon, and some new effects are present in single event transients (SETs) due to the charge sharing collection of the adjacent multiple-transistors. In this paper, not only the off-state p-channel metal-oxide semiconductor field-effect transistor (PMOS FET), but also the on-state PMOS is struck by a heavy-ion in the two-transistor inverter chain, due to the charge sharing collection and the electrical interaction. The SET induced by striking the off-state PMOS is efficiently mitigated by the pulse quenching effect, but the SET induced by striking the on-state PMOS becomes dominant. It is indicated in this study that in the advanced technologies, the SET will no longer just be induced by an ion striking the off-state transistor, and the SET sensitive region will no longer just surround the off-state transistor either, as it is in the older technologies. We also discuss this issue in a three-transistor inverter in depth, and the study illustrates that the three-transistor inverter is still a better replacement for spaceborne integrated circuit design in advanced technologies.     

硅微机械陀螺传感器信号的检测方法

硅微机械陀螺是近几年发展起来的一种新型惯性元件。由于其巨大的军事和民用价值,各国均将研制过程中的关键技术列为高度机密。本文对硅微机械陀螺的关键技术之一 传感器信号的检测方法进行了探讨。提供了几种硅微机械陀螺传感器信号的检测方法,并对这几种检测方法进行了比较。     

“正确证明”有瑕疵

第32届IMO试题如图1,P为△ABC内任意一点,求证:∠1,∠2,∠3中至少有一个不大于30°本刊2009年第10期高群安老师给出错误证明后,笔者在本刊2010年第6期予以纠正如下:证明假设∠1,∠2,∠3都大于30°,设P点到三角形三边AB、BC、CA的距离分别为p,q,r,则PA<2p,PB     

Experimental verification of the parasitic bipolar amplification effect in PMOS single event transients

The contribution of parasitic bipolar amplification to SETs is experimentally verified using two P-hit target chains in the normal layout and in the special layout. For PMOSs in the normal layout, the single-event charge collection is composed of diffusion, drift, and the parasitic bipolar effect, while for PMOSs in the special layout, the parasitic bipolar junction transistor cannot turn on. Heavy ion experimental results show that PMOSs without parasitic bipolar amplification have a 21.4% decrease in the average SET pulse width and roughly a 40.2% reduction in the SET cross-section.     

国外动调陀螺仪再平衡技术的发展

本文在综合大量文献的基础上，详细介绍了国外模拟、数字再平衡技术的发展过程以及现阶段研究状况。同时，对动力调谐陀螺仪模拟、数字再平衡回路进行了分析比较，归纳了两者的主要优缺点。另外，还简略介绍了直接数字控制技术。     

自适应联邦滤波器及其在组合导航系统中的应用

针对现有的信息分配方法在滤波精度和自适应性方面存在不足的问题,设计了一种在模糊神经网络基础上改进的自适应联邦滤波器,利用模糊神经网络自适应地调整信息分配系数,从而有效抑制干扰对子滤波器工作状态的影响,使主滤波器能够充分、有效地利用子滤波器的信息。将这种自适应联邦滤波器应用到MINS/GPS组合导航系统设计中,并对系统进行了仿真。通过与基于常规联邦滤波器的组合系统的仿真结果比较可知,自适应联邦滤波器的组合系统在性能上有了显著的提高,且速度误差标准差控制在0.06m/s以内,位置误差标准差控制在3.3m以内,具有良好的导航精度。