一种新型的切削数据优化方法

切削数据是度量切削技术水平高低的基本量值，采用优化的切削数据是发挥机床功能，提高切削效率的基本方法，目前，已有的切削数据优化方法存着计算步骤繁复、优化时间长等缺点，难以满足现代制造技术发展的需要。本文在给出目标函数和约束条件一般形式的基础上利用ｆ最小线，ｖ最小线和ｚ等值线等概念提出了单工序下通用的切削数据优化方法－目标等值线法，该方法不需进行迭代运算，计算简单，与通常的优化方法相比，其优化速度提高     

惯导系统在轮式自行火炮中的应用

分析了轮式自行火炮发展过程中所应用的惯导系统的结构原理,总结了不 同结构方案的惯导系统的优缺点,展望了应用于轮式自行火炮的导航系统的发展方向, 为新型地面火炮的操作使用、技术勤务以及升级改造提供理论依据和参考。     

进气道物面贴体坐标生成的几何自适应控制方法

针对轴对称进气道跨音速绕流问题的特点,用几何自适应的方法和椭圆型方程构筑了适合流场特征的贴体坐标系,并用AF3格式计算了A－27进气道物面上的压力分布。计算结果表明：几何自适应方法能够控制进气道物面上网点的疏密,给出进气进物面上网点的良好分布,从而为进气道跨音速绕流问题的准确计算奠定了基础。     

光学4F系统象平面附近光强分布的研究

首先推导出光学４Ｆ系统的一般衍射变换公式，用不透明圆盘模型算出了象平面附近三维空间内的光强分布。根据计算结果，定义了象的归一化半径和象的变缘锐化率，给出了它们与粒子离物平面远场数之间的关系，从而定量地得出成象区、失真区和远场区的物理图象。最后，对粒子场测量中的粒径和空间位置测量的最小误差作了讨论。这些结果，对分析粒子的大小和分布是十分重要的，并在喷嘴雾化场测试中得到了应用。     

New progress on space solar telescope

The design of the Space Solar Telescope (phase B) has been completed. The telescope system has been manufactured (phase C) since the beginning of 1999, and it will be assembled by the end of 2000. In this paper, mainly the optical design, technique and manufacture will be described. The launch is planned for the summer of 2004.     

我国民营快递企业发展的对策

我国民营快递企业经过二十年的发展,取得了长足的进步,已经在国内快递市场占有了一席之地。但面对国有快递企业及外资快递企业的竞争时,民营快递企业自身存在的劣势将成为其进一步发展壮大的阻碍。通过对民营快递企业的内外部环境分析,明确民营快递企业的优势与劣势,找到外部环境中的机会与威胁,并提出了民营快递企业发展的具体策略。     

Adaptive array CFAR detection

Presented here is a large class of adaptive array detection algorithms with constant false alarm rate (CFAR), so that the false alarm rate can be set to any preassigned number without knowledge of the noise covariance matrix. This class map incorporate any usual method of cell averaging and any method for array weight vector synthesis. A sufficient condition for CFAR is derived, which is easy to satisfy in practice. Basic system parameters are discussed. An example of detection performance for a simple cell-averaging detector, in which the array weight vector is synthesized by the method of diagonal loading, is provided using Monte Carlo simulations     

8"×8" full color cockpit display

The operation of active matrix liquid crystal displays (AMLCDs), the preferred flat-panel displays for avionic and aerospace applications, is explained. An 8-in.×8-in. full-color AMLCD designed for a military aircraft is described, as well as the principles of the p-i-n diode switch on which its design is based. The performance characteristics of the display are examined     

Optimal Utilization of Satellite Communication Systems through Supervisory Control

Users of satellite communication systems being designed are charcterized by diversity. System designers now have the capability of serving thousands of simultaneous users; the users need not all follow the same system parameters. Diversity and characteristics are shown, and an attempt is made to list all the parameters desired by users. Usage of satellite communications systems is projected to serve a maximum of 200 000 users by means of 10 multipurpose satellites. It is shown that a supervisory control system is necessary to achieve optimal utilization of the existing resources.