时间频率的高准确度测量方法

论述了目前时间频率在时域的高准确度测量中所采用的标准及测量技术与方法。我们组建的时间频率标准自动测试系统和时间频率标准相位比较测量系统,其准确度分别为1×10-12和2×10-14/d。     

ZrB2 粉体制备技术的研究进展

综述了国内外ZrB2粉体制备技术如固相法、液相法和气相法的研究进展,详细分析了各种制备技术的特点,并展望了ZrB2粉体制备技术的发展方向。     

Solar Energetic Particle Charge States: An Overview

The ionic charge distributions of solar energetic particles (SEP) as observed in interplanetary space provide fundamental information about the origin of these particles, and the acceleration and propagation processes at the Sun and in interplanetary space. In this paper we review the measurements of ionic charge states of energetic particles in interplanetary space and discuss their implication for our understanding of SEP sources, and acceleration and propagation processes.     

薄膜充气管展开模拟试验

根据多体理论中凯恩方法建立的折叠充气管模型,模拟研究了V形折叠充气管的充气展开动力学特性.由管内气压变化与充气展开时间的关系,分析了不同充气速率和初始展开角时展开加速度与时间的关系.结果表明:该模拟方法有效,展开加速度与充气速率总体成正比.另发现,为改善充气管的展开动力学性能,需控制特定展开角度范围内的加速度波动.     

基于高频光电导法半导体少数载流子寿命测量系统的设计与实现

基于高频光电导衰减法半导体少数载流子寿命测量基本原理,设计了半导体少子寿命测量系统,并在二极管检波电路的基础上,对信号处理系统进行了改进。该信号处理系统采用反馈式检波电路,相比于传统二极管检波电路,运用运算放大器的反馈原理减小了检波二极管压降产生的误差,同时结合二极管嵌位作用,减小了运算放大器压摆率带来的影响,提高了测量系统的检波能力。通过实验,验证了该检波电路的可行性,测试结果表明,有效提升了测量系统的准确性。     

Testing the improvement of performance of the IRI model in the estimation of TEC over the mid-latitude American regions

This paper mainly discusses the improvement of performance of the International Reference Ionosphere (IRI) model in estimating the variation of the Vertical Total Electron Content (VTEC) over the mid latitude American regions during the relatively low (2008–2010) and relatively high (2012) solar activity years. This has been conducted employing the VTEC values obtained from the dual frequency ground based Global Positioning System (GPS) receivers located at Mineral Area Community College, MACC (37.85°N, 269.52°W) and Mississippi County Airport, MAIR (36.85°N, 270.64°W), and the latest versions of the IRI online model (IRI 2007, IRI 2012 and IRI 2016). The study mainly focuses to compare the trend of variability of the monthly and seasonal modeled VTEC values (IRI 2007 VTEC, IRI 2012 VTEC and IRI 2016 VTEC) with the corresponding measured VTEC values (GPS VTEC). The overall results show that the IRI VTEC values (almost in all versions of the model) are generally smaller than the GPS VTEC except after about 15:00 UT (09:00 LT) in the December solstice when the Sun shifts to the high solar activity. On the contrary, overestimations of the VTEC values by the model are observed in traversing from the low solar activity (2008) to high solar activity (2012) phase, especially after about 15:00 UT (09::00 LT) with the IRI 2016 version showing the highest. In general, the IRI 2007 and IRI 2012 versions show similar monthly and seasonal underestimations or overestimations showing that the two versions have almost similar performance. The IRI 2016 version is generally better in capturing both the diurnal and arithmetic mean GPS VTEC values with some exceptional months and seasons as compared to those of the IRI 2007 and IRI 2012 versions.     

基于XTCE标准的遥测参数装订与核对研究

面对我国现代航天高密度发射的需求,精准高效的遥测参数装订与核对尤为重要。本文基于XTCE标准定义的遥测参数格式,构建了XTCE标准对遥测参数数据底座,实现遥测参数的统一标准、统一管理和统一平台。阐述了XTCE标准的结构、火箭遥测数据库的生成和数据底座的构造。实现了对大型火箭遥测参数的自动装订,大幅提高了工作效率。     

摩擦热效应对航空发动机高压转子系统碰摩响应的影响

以航空发动机高压转子为研究对象,采用有限元法建立了考虑摩擦热效应的高压转子热碰摩动力学模型。研究了高压转子的摩擦生热和摩擦热碰摩响应特性,并和未考虑摩擦热效应的碰摩响应进行了对比分析。结果表明,当考虑摩擦热效应时高压转子的最大碰摩力显著增大,碰摩频率也明显增加。高压转子呈现出明显的非线性碰摩特征,同时各结点的最大振幅均比忽略摩擦热效应的最大振幅有不同程度的增大。在实际工程问题中,不应当忽略碰摩热效应对碰摩响应的影响。     

高维不确定性条件下飞行器级间分离可靠性评估

针对高维不确定性条件下飞行器级间分离精细化分析需求,建立参数化级间分离动力学仿真模型,综合考虑级间分离过程中高维不确定性因素影响,识别典型分离失效模式,构建分离可靠性模型.提出采用活跃子空间方法实现高维不确定性参数的空间降维,结合极大极小距离序贯采样方法,利用含交叉项的高阶多项式回归模型对降维空间进行近似,完成了可靠性...     

一种高动态频率跟踪环路的数字实现与分析

在弹载无线制导系统中,由于导弹的高动态特性,导致接收机所接收信号具有显著的多普勒频移。围绕载波频率跟踪环路的研究多在低动态环境下开展。针对高动态、低信噪比环境下接收信号的载波捕获与跟踪问题,提出了一种结合频率修正环节的载波频率跟踪环路,并重点分析了环路中叉积自动频率跟踪算法和高阶环路滤波器的特点。实验结果表明了该环路能够完成高动态环境下的频率跟踪。