信息度量在图像数据压缩中的应用

假设目标和系统噪声过程正态分布、空间平稳、遍历、统计独立且均方意义可加,单位像素传输的目标信息量将无损条件下的极限编码宽度同目标统计特征、系统调制传递函数和信号噪声比联系了起来.仿真计算表明,信号噪声比是决定极限编码宽度的主要因素.     

框架零件的加工

论述了ZTC4框架零件的加工特点与主要表面精度的加工方法、各项工艺参数的选择、质量控制及工序间的冷热处理的要求,为框架类零件的加工积累了经验。     

快变分量观测与基本分量特性

本文对太阳２２周峰年期云南天文台日冕射电频谱仪观测到的６０个快速事件作了分析。从中获得了尖峰辐射、增强噪暴、快速起伏、类尖峰、叠加脉冲五种快变型别，对它们的亮温度、叠加特性、特征时间、辐射源尺度、偏振特性以及辐射机制六个方面作了分析研究后，对射电爆发、缓变分量和宁静太阳的辐射特征参量也作了研究，从而得出基本分量特性。     

超音轴向分速风扇/压气机叶栅流动特征分析

本文介绍了三种带冲波的超音轴向分速叶型设计,及其叶栅流场计算,分析了这些叶栅流场特征。在计算的反压条件下,全部波系均控制在槽道内,叶栅槽道内存在不同大小的轴向分速超音区,这种叶型叶栅可承受的增压比高,总压恢复系数较低,这类叶栅的性能和流动特征尚缺少实验数据和理论分析。     

复合材料夹层圆柱壳的轴对称失稳问题

本文首先给出复合材料夹层圆柱壳大挠度问题的一般方程,然后在轴对称变形条件下进行简化,得到轴对称变形的非线性方程。在此基础上用摄动法,给出了复合材料夹层圆柱壳轴压轴对称屈曲方程,该方程与齐次边界条件一起构成分析轴对称失稳的特征值问题。通过详细分析得到了该特征值问题的解,无量纲的轴压临界值表达成无量纲的抗弯刚度参数,夹芯抗剪刚度参数和Badtoff几何参数的简单函数。通过这些无量纲参数,轴压临界值实际上是复合材料工程弹性常数,夹心横向剪切模量,各层纤维铺设角,铺层数,夹心相对于表层的厚度和圆柱壳参考中面几何尺寸的函数。     

基于主成分分析的航天企业风险评价研究

基于我国我数航天企业正处于从计划经济到市场经济转轨阶段的现实，对比航天企业经济效益综合评估的诸多方法，综合考虑主成分分析法具有全面性、可比性、合理性和可行性等优点，建立了一套较为科学的航天企业风险评价方法，即在确立航天企业风险评价指标体系的基础上，运用主成分分析方法对风险指标体系进行科学的分析化筒，通过资信评价对航天企业风险状况展开评判。最后，结合实例作了进一步具有的说明。     

Use of principal component analysis in the identification of the spatial pattern of an ionospheric total electron content anomalies after China’s May 12, 2008, M = 7.9 Wenchuan earthquake

This paper uses principal component analysis (PCA) to determine the spatial pattern of total electron content (TEC) anomalies in the ionosphere post the China’s Wenchuan Earthquake of 12 May, 2008 (UTC) (M_w = 7.9). PCA and image processing are applied to the global ionospheric map (GIM) with transforms conducted for the time period 08:00–10:00 UT on 12 May 2008. Results show that at a height of approximately 200 km the anomaly is widespread and less intense; however, it becomes more localized with height reaching maximum intensity and localization at an altitude of 300 km. The spatial distribution is remarkably similar to that reported for a TEC anomaly previously identified as a precursor anomaly on May 9, 2008 for the same time period. Potential causes of the results are discussed with emphasis given to vertical acoustic gravity waves based on the spatial pattern identified.     

The IGY and beyond: A brief history of ground-based cosmic-ray detectors

The state of art of ground-based cosmic-ray research from its discovery to present is reviewed. After discovery of cosmic rays by Hess in 1912, the nature of the primary and secondary radiation was established from recordings by a variety of instruments, sensitive to various components of cosmic rays and operated at different latitudes, longitudes and altitudes, including instruments carried by balloons. The IGY formalized international co-operation and coordinated study of cosmic rays, which is vital for meaningful interpretation of cosmic-ray data. Data collected at different geographic locations require an effective cutoff rigidity as a data ordering parameter. This parameter is obtained from tracing trajectories of primary cosmic rays in the Earth’s magnetic field. After 50 years the world’s neutron monitor network remains still the backbone for studying intensity variations of primary cosmic rays in the rigidity ranges between 1 and 15 GV, associated with transport and with transient events. Also the penetrating muon and neutrino components of secondary cosmic rays have a long history of recording and fundamental problem investigations. Valuable data about composition and spectrum of primary cosmic rays in ever increasing high-energy regions have been obtained during the years of investigations with various configurations and types of extensive air shower detectors. The culture of personal involvement of the physicist in carrying out experiments and data acquisition characterized the continued vitality of cosmic-ray investigations ranging from its atmospheric, geomagnetic and heliospheric transport through to its solar and astrophysical origins.     

空气系统对核心机性能敏感性的影响

为了确定空气系统不同位置引气量对核心机性能的影响，给总体性能和空气系统设计提供依据，以某型核心机设计过 程为例，将空气系统设计迭代到总体性能设计中，研究了空气系统对核心机性能和部件特性的影响，并开展了空气系统对核心机 性能的敏感性分析。结果表明：每个引气位置引气量的增加均会导致燃烧室出口温度的升高，其中用于涡轮转子冷却的引气对燃 烧室出口温度的影响最大，其次为第5级压气机引气，再次为用于涡轮导向器冷却的引气，影响最小的为用于涡轮后机匣冷却的 引气。将空气系统设计结果迭代到核心机性能模型中，迭代后的压气机和涡轮工作特性发生了变化，压气机共同工作线受引气量 增加的影响稍微下移，涡轮落压比由于燃烧室出口温度的升高而减小。     

基于FFDiag算法的变步长盲信号分离

基于快速Frobenius联合近似对角化（FFDiag）算法,提出了一种步长根据代价函数值大小变化的更新规则,使对角化的更新幅度随信号分离状态自适应变化。算法步长与信号分离状态相结合,具有收敛速度快和稳态误差小双重优点,仿真结果证实了算法的有效性。