太阳射电微波爆发的频谱分析

1981年4月1日太阳发生一个4N级Hα耀斑并伴随出现强烈的IV型射电爆发.本文对北京天文台,西澳大利亚站等射电资料进行分析.分析表明:(1)该事件的微波源状态相对稳定,米波源位置存在移动,因此产生微波辐射与米波辐射是两组不同的电子群体,在爆发频谱指数的时变曲线上表现出明显的形态差异.还由于两者辐射源的位置不同,微波与米波的爆发在峰值时刻上也不完全符合.(2)4月1日微波大爆发是由三个主爆发组成的,它们的峰值时刻分别为0135.1,0146.1,0153.6UT.由射电高频端谱指数算出的非热电子能谱指数表明,在射电爆发的三个峰值时刻电子能谱都变硬.本文还得出该活动区的非热电子平均速度(以光速c为单位)β为0.9左右,磁场强度B为430G.并由回旋同步辐射阻尼算得,非热电子的寿命为829秒,这个数值与三个主峰的持续时间相吻合.     

复合材料层合残余应力实验研究

取单向板90°试样用DMA法测出的玻璃化温度T_(?)为应力释放温度,用应变片包埋法测定了玻纤/648环氧复合材料单向试样与对称正交层板的热应变,用经典层板理论处理实验结果,实验值与理论值吻合;结果还表明,一般意义上的复合材料内的层合残余应力与制造过程中复合材料内的残余应力应作区别。     

余辉等离子体的实验研究

利用调制脉冲产生的余辉等离子体的参数测量表明:等离子体空间电位和电子温度的衰变是重要的,它在余辉等离子体的密度衰变过程研究中必须予以考虑.对容器中余辉等离子体密度径向分布的测量结果与理论预言是一致的.     

微波泄漏对光抽运铯束频标准确度影响的分析

微波泄漏是影响光抽运铯原子钟准确度的主要因素之一. 傅里叶变换分析法是分析其影响的主要手段,但该方法只能用来分析有效原子速度分布很窄的情况.通过分析和计算,推导出频移随漏场的位置、相位和幅度变化的关系式.计算和分析的结果表明,漏场引起频移大小和漂移区的长度、输入微波功率值和漏场的相位、强度和位置等有关.所得的结果和用傅里叶变换方法分析所得的结果是一致的,分析的方法不受原子有效速度限制.     

多传感器信息融合技术

多传感器信息融合是Ｃ＾３Ｉ系统和电子综合战系统中的关键技术，本文从信息融合分类出发，讨论了单传感器的信息融合决策理论和技术以及多传感器信息融合原理，提出了多传感器信息融合专家系统，着重讨论贝叶斯法用于二元检测的分布式多传感器信息融合的检测方式。     

新媒体视域下系统构建“三位一体”公寓管理模式

随着科技日益进步和5G时代的即将到来,在治理体系上越来越注重管理与哲学教育相结合,高校作为接收新事物、新思维的前沿阵地。学生公寓成为大学生思想政治教育的又一个重要的阵地,因此创新公寓管理体系并努力做到使之与哲学相结合也成为了一项重大任务,高校辅导员、公寓辅导员、高校后勤管理人员结合新媒体创新学生公寓的管理方式对新时代大学生的教育、管理、服务掌控和开展思想政治教育工作至关重要。     

A comprehensive study of the 2016 Mw 6.0 Italy earthquake based on high-rate (10 Hz) GPS data

The 2016 M_w 6.0 Italy earthquake is successfully recorded by the near-field 10?Hz GPS and 200?Hz Strong Motion (SM) stations, providing valuable data for this study. A comprehensive study of this earthquake is carried out based on GPS data, which contains coseismic deformations analysis, noise analysis, seismic wave picking, and magnitude determination. The noise of most GPS-derived displacement waveforms can be described as a combination of white noise, flicker noise, and random walk noise after the earthquake occurrence, and the spectral indices vary significantly for most stations, implying that the seismic signals have affected the noise characteristic of GPS-derived displacement waveforms. S-transform is employed to assess the GPS capability to detect the seismic arrival time. The SM station AMT and the GPS station AMAT are in good agreement in seismic wave picking, and the difference is only 1.2?s in the north component, suggesting that the outcome of seismic wave picking using GPS data is reliable. Then, a classic empirical formula is employed to determine the moment magnitude. A robust moment magnitude (Mw 5.90) can be estimated by the nine GPS stations with about 23.9?s. If four GPS stations near the epicenter is chosen to determine the magnitude, it only take 13.0?s to retrieve a reliable preliminary (Mw 5.82) magnitude, which is 5.4?s ahead of nine stations. In addition, Cross Wavelet Transform (XWT) is adopted to measuring the correlation and phase relationship between GPS and SM records. The result of XWT analysis indicates 10?Hz GPS is capable of capturing reliable and accurate coseismic dynamic deformations, as evidenced by the XWT-based semblance being close to 1 between GPS and SM records. The above results confirm the capability of 10?Hz GPS to capture coseismic dynamic deformations, detect seismic arrival time, and determine earthquake magnitude. Moreover, rapid magnitude determination based on 10?Hz GPS data can be regarded as an important supplement to Earthquake Early Warning (EEW).     

李宏新发动机设计专家

作为长期从事飞机发动机研发工作的中航工业首席技术专家,请您谈一谈我国飞机发动机的研发现状以及需要攻克的难关。李宏新:航空发动机的研制是一个复杂的系统工程,研制道路充满艰辛和坎坷,不容丝毫懈怠和疏忽。     

A general calculation method to specify center-of-buoyancy for the stratospheric airship with multiple gas cells

As the lighter-than-air (LTA) flight vehicle, the stratospheric airship is a desirable platform to provide communication and surveillance services. During the ascent from sea-level to the mission altitude, the volume of the lifting gas may change significantly, which will result in the change of the center-of-buoyancy (CB). A general calculation method is developed to specify CB for the stratospheric airship with a double-ellipsoid hull and an arbitrary number of the gas cells. The cross-section-integral (CSI) method is used as a basic calculation scenario to specify CB. Considering the complexity in determining the boundary between the helium and air in the gas cell, a searching algorithm is put forward and the specification of CB can be conducted by the iterative calculation. As an important application, the stable condition of the pitch angle is analyzed when the change of CB is involved. Under different initial configurations, the stable pitch angle of the stratospheric airship during the ascent is specified and compared, which shows the advantages of the multi-gas-cell configuration. The results of this paper may provide an important reference for the engineering application of the stratospheric airship.