浅谈法治边检建设

＂法治边检＂建设是在党的十八届三中全会提出建设＂法治中国＂目标时代背景下,在提高边检服务水平工作进入深水区、社会各界对边检工作要求日趋严格和多样化形势下,边检机关立足工作实际,顺应时代发展的必然选择。分析＂法治边检＂的理论内涵和面临形势,总结法治边检建设现状和存在问题,从构建体系型边检、有限型边检、效能型边检、责任型边检、服务型边检、信用型边检、开放型边检、廉洁型边检等方面对法治边检体系建设进行了探讨。     

基于单变量多目标规划的装甲车辆冷却系统智能化控制

根据新一代装甲车辆推进系统热部件散热特点及其冷却系统调控原理,提出了一种单变量多目标数学规划与模糊智能控制相结合的控制算法。该算法将冷却系统抽象为单变量多目标数学规划问题,采用加权的方法将多个目标函数转化为综合目标函数,输入到模糊智能控制器中进行冷却控制。仿真结果表明:该控制算法具有良好的控制效果,能够有效地解决新型推进系统热源多、目标温度范围广而可调参数单一的问题。     

The legality of unmanned aerial vehicles outside the combat zone: a case study of the Federally Administered Tribal Areas of Pakistan

The drone is the latest tool to promote interests of a nation-state. It is clear that USA as well as other major powers anticipate that robotics will play a key role in future warfare. Today, more than 70 countries have already acquired drone technology and many others are desperate to join the ranks. This urge for drone technology will ultimately lead to a “boundless and borderless war without end.” In the case of Pakistan, the US drone campaign has raised some important issues regarding how their use could, or should, be regulated in the future. This article analyses the legal issues raised by the US's use of drone technology in non-combat zones, such as Pakistan. It is argued that a reckless disrespect of Pakistan's sovereignty has had adverse implications and consequences for the legitimacy of the Pakistani government. Drone strikes have prompted instinctive opposition among the Pakistani population, hurt their feelings and estranged them from the government. This in turn has added to Pakistan's instability and stimulated a ground-swell of animosity toward the USA.     

BTT导弹制导律研究综述

与STT导弹相比,BTT导弹在气动效率、机动能力、控制性能等方面具有明显优势,但其运动耦合特性也给传统研究框架下的制导律设计带来了挑战。本文针对BTT导弹制导律设计问题展开研究,首先描述了BTT导弹制导基本问题,分析了BTT导弹制导律设计的技术难点,需要综合考虑运动耦合、多约束、目标机动、弹体动态效应等因素,然后综述了国内外现代制导律设计的基本方法,将其分为双通道解耦法、球坐标法、现代几何法等,最后指出了BTT导弹制导律的进一步研究方向。     

AFRICAN REGIONAL ORGANISATION' PEACE OPERATIONS

This paper reviews recent developments among African regional organisations in undertaking peacekeeping operations, as well as in preparing for future missions. It focuses on those that have been the most active: the Organisation of African Unity/African Union, the Economic Community of West African States and the Southern African Development Community. The paper goes on to briefly describe and analyse the activities of the French, UK, and US capacity-building programmes designed to develop African peacekeeping capacities. The author then identifies some specific concerns and recommends actions to help meet today's challenges. The paper concludes with a short analysis of African organisations' capacities and proclivities to provide a peacekeeping force for Sudan.     

再生冷却通道结构参数对碳氢燃料流量分配影响

以液体火箭发动机再生冷却技术为背景,采用数值模拟方法对Z-type型并联通道流量分配特性进行研究,分析了通道数、通道截面形状及入口汇流结构对流量分配特性的影响。研究结果表明:在冷却通道总流通面积相同的情况下,随着再生冷却系统通道数的增加,流量分配不均匀度系数从2.59%降低至0.5%,相同流通面积下增加通道数可以有效提高流量分配的均匀程度。通道截面形状对流量分配不均匀度系数影响不大,其影响主要表现在通道内部流体速度分布及换热面积上。从换热效果看,梯形截面构型要优于矩形构型。入口汇流结构倾斜角有利于流量的均匀性分布。该研究对于再生冷却通道结构设计具有一定参考价值。     

气氧/煤油发动机水冷推力室壁热分析

针对气氧／煤油地面试验发动机的热防护问题，采用非定常三维壁温分布模型为主体的分析模型，对槽道式水冷推力室壁温特性进行了计算分析。燃气流与冷却水流采用一维流动模型计算。应用有限差分方法确定了燃气与室壁的换热热流、推力室壁温分布，给出了壁温随时间变化的规律，讨论了冷却水流量对壁温的影响。     

液体火箭发动机烧蚀冷却推力室室壁温度响应的计算

本文对液体火箭发动机烧蚀冷却推力室的冷却机理进行了分析,较为全面地考虑了影响温度场的主要因素,利用六点中心差分建立了离散数学模型,并对室壁温度响应进行了计算,得到了烧蚀速率和侵蚀速率等。所得结果可供设计推力室时参考。     

载人飞船上升段轨道的Newton迭代设计法

本文对载人飞船上升段轨道的一种工程设计方法进行了探讨。该方法的特点是根据上升段飞行的特征,运用飞行力学原理选定其控制规律的数学模型,然后根据上升段轨道的中间约束条件和终端约束条件,利用Newton迭代法确定模型中的各待定参数。本文给出了该设计方法的流程图,并通过模拟计算论证了该设计方法的可行性。