Optimal control for multi-servers queueing systems under periodic review

This paper deals with the problem of finding the optimal dynamic operating policy for an M/M/S queue. The system is observed periodically, and at the beginning of each period the system controller selects the number of service units to be kept open during that period. The optimality criterion used is the total discounted cost over a finite horizon.     

基于Ansofl的PMLS发电机纵向边端效应仿真

永磁直线同步发电机特殊的结构使其存在一种特殊现象——纵向边端效应,从而严重影响了永磁直线同步发电机的性能。利用有限元电磁场分析软件Ansoft建立了永磁直线同步发电机的二维模型,分析了纵向边端效应产生的原因,以及纵向边端效应对永磁直线同步发电机初级磁场的影响。利用磁阻相等的原理,通过增加发电机端部齿宽度和极数两种方法来改善永磁直线发电机性能。经Ansoft软件仿真,结果表明增加端部齿宽度和极数可以有效抑制纵向边端效应,提高永磁直线同步发电机的性能。     

战术互联网中的视频传输技术

介绍了战术互联网,阐述了视频传输技术的简单原理和基本特点,分析了视频传输在战术互联网中的几种传输技术。     

未知雷达位置参数识别研究

在对国内外数据融合方面研究进展情况进行分析的基础上,提出了一种应用模糊关联、数据融合和最小二乘等技术识别未知雷达辐射源具体坐标的方法,为进一步融合未知源的数据打下基础。仿真结果表明,随着采样数据的增加,对辐射源参数的估计会更加精确。     

潜艇结构强度研究的新近进展

本文从结构材料、结构形式、非线性分析、组合壳体和端盖强度以及结构的减振降噪等方面论述了潜艇结构强度研究的新近进展,并指出了今后的研究方向。     

关于排水型两栖车辆水上航速的研究

本文引入造船学的有关理论,从理论和实验基础上研究履带式排水型两栖车辆水上航行所遇到的阻力,以形状阻力和兴波阻力为主.高速航行时,兴波阻力上升为主要阻力成份,它是阻碍排水型两栖车辆水上航速提高的主要原因,由此文中提出了排水型两栖车辆水上实用极限速度问题.     

Influence of a liquid-filled compartment structure on the incoming shaped charge jet stability

Liquid-filled compartment structure consists of a bulk steel plate with matrix blind holes which are filled with liquid and a steel front plate to seal up the liquid with rings and bolts.The liquid-filled compart-ment structure can resist the shaped charge warhead effectively.This paper presents experimental and theoretical investigations of the penetration ability of the residual shaped charge jet emerging from the liquid-filled compartment structure after the penetration process at different impact angles.On the basis of shock wave propagation theory,the influence of the liquid-filled compartment structure on jet sta-bility is analysed.The interferences of the liquid backflow caused by a reflected shock wave and a back plate on jet stability under different impact angles are also examined.In addition,the range of the disturbed velocity segments of the jet at different impact angles and the penetration ability of the re-sidual jet are obtained.A theoretical model is validated against the experimental penetration depths.     

An experiment evaluating how the tiny mass eccentricities in spin-stabilized projectiles affect the position of impact points

This study investigates and quantifies some possible sources affecting the position of impact points of small caliber spin-stabilized projectiles (such as 12.7 mm bullets). A comparative experiment utilizing the control variable method was designed to figure out the influence of tiny eccentric centroids on the projectiles. The study critically analyzes data obtained from characteristic parameter measurements and precision trials. It also combines Sobol's algorithm with an artificial intelligence algorithm—Adaptive Neuro-Fuzzy Inference Systems (ANFIS)—in order to conduct global sensitivity analysis and determine which parameters were most influential. The results indicate that the impact points of projectiles with an entry angle of 0° deflected to the left to that of projectiles with an entry angle of 90°. The difference of the mean coordinates of impact points was about 12.61 cm at a target range of 200 m. Variance analysis indicated that the entry angle — i.e. the initial position of mass eccentricity — had a notable influence. After global sensitivity analysis, the significance of the effect of mass eccentricity was confirmed again and the most influential factors were determined to be the axial moment and transverse moment of inertia (Izz Iyy), the mass of a projectile (m), the distance between nose and center of mass along the symmetry axis for a projectile (Lm), and the eccentric distance of the centroid (Lr). The results imply that the control scheme by means of modifying mass center (moving mass or mass eccentricity) is promising for designing small-caliber spin-stabilized projectiles.     

Mitigation effects on the reflected overpressure of blast shock with water surrounding an explosive in a confined space

The mitigation of blast shock with water has broad application prospects. Understanding the mitigation effects on the reflected overpressure of the explosion shock with water surrounding an explosive in a confined space is of great significance for military explosives safety applications. To estimate the effects of the parameters on the reflected overpressure of blasted shock wave, a series of experiments were carried out in confined containers with spherical explosives immersed in a certain thickness of water, and numerical simulations were conducted to explore the corresponding mechanisms. The results reveal that the reflected overpressure is abnormally aggravated at a small scaled distance. This aggravation is due to the high impulse of the bulk accelerated water shell converted from the explosion. With increasing scaled distance, the energy will be gradually dissipated. The mitigation effects will appear with the dispersed water phase front impacting at a larger scaled distance, except in the case of a dense water phase state. A critical scaled distance range of 0.7—0.8 m/kg1/3 for effective mitigation was found. It is suggested that the scaled distance of space walls should be larger than the critical value for a certain water-to-explosive weight ratio range (5—20).