5GHz雷达的干扰计算模型概述

文章从开发5 GHz模型的目的入手,简要介绍了5 GHz模型的结构组成,详细讨论了5 GHz模型的干扰计算流程,包括无线局域网和雷达的场景设置、技术参数设置、总干扰计算等,最后给出了5 GHz模型的一个运行范例,以期为其它干扰模型的开发提供借鉴参考。     

Effects of nano-sized aluminum on detonation characteristics and metal acceleration for RDX-based aluminized explosive

Nano-sized aluminum(Nano-Al)powders hold promise in enhancing the total energy of explosives and the metal acceleration ability at the same time.However,the near-detonation zone effects of reaction between Nano-Al with detonation products remain unclear.In this study,the overall reaction process of 170 nm Al with RDX explosive and its effect on detonation characteristics,detonation reaction zone,and the metal acceleration ability were comprehensively investigated through a variety of experiments such as the detonation velocity test,detonation pressure test,explosive/window interface velocity test and confined plate push test using high-resolution laser interferometry.Lithium fluoride(LiF),which has an inert behavior during the explosion,was used as a control to compare the contribution of the reaction of aluminum.A thermochemical approach that took into account the reactivity of aluminum and ensuing detonation products was adopted to calculate the additional energy release by afterburn.Combining the numerical simulations based on the calculated afterburn energy and experimental results,the param-eters in the detonation equation of state describing the Nano-Al reaction characteristics were calibrated.This study found that when the 170 nm Al content is from 0％to 15％,every 5％increase of aluminum resulted in about a 1.3％decrease in detonation velocity.Manganin pressure gauge measurement showed no significant enhancement in detonation pressure.The detonation reaction time and reaction zone length of RDX/Al/wax/80/15/5 explosive is 64 ns and 0.47 mm,which is respectively 14％and 8％higher than that of RDX/wax/95/5 explosive(57 ns and 0.39 mm).Explosive/window interface velocity curves show that 170 nm Al mainly reacted with the RDX detonation products after the detonation front.For the recording time of about 10 μs throughout the plate push test duration,the maximum plate velocity and plate acceleration time accelerated by RDX/Al/wax/80/15/5 explosive is 12％and 2.9 μs higher than that of RDX/LiF/wax/80/15/5,respectively,indicating that the aluminum reaction energy significantly increased the metal acceleration time and ability of the explosive.Numerical simulations with JWLM explosive equation of state show that when the detonation products expanded to 2 times the initial volume,over 80％of the aluminum had reacted,implying very high reactivity.These results are significant in attaining a clear understanding of the reaction mechanism of Nano-Al in the development of aluminized explosives.     

Automated integration of real-time and non-real-time defense systems

Various application domains require the integration of distributed real-time or near-real-time systems with non-real-time systems.Smart cities,smart homes,ambient intelligent systems,or network-centric defense systems are among these application domains.Data Distribution Service(DDS)is a communi-cation mechanism based on Data-Centric Publish-Subscribe(DCPS)model.It is used for distributed systems with real-time operational constraints.Java Message Service(JMS)is a messaging standard for enterprise systems using Service Oriented Architecture(SOA)for non-real-time operations.JMS allows Java programs to exchange messages in a loosely coupled fashion.JMS also supports sending and receiving messages using a messaging queue and a publish-subscribe interface.In this article,we pro-pose an architecture enabling the automated integration of distributed real-time and non-real-time systems.We test our proposed architecture using a distributed Command,Control,Communications,Computers,and Intelligence(C4I)system.The system has DDS-based real-time Combat Management System components deployed to naval warships,and SOA-based non-real-time Command and Control components used at headquarters.The proposed solution enables the exchange of data between these two systems efficiently.We compare the proposed solution with a similar study.Our solution is superior in terms of automation support,ease of implementation,scalability,and performance.     

GPS弹道修正引信弹道环境信息的解算与数值仿真分析

根据质点弹道的特点, 描述了弹目间距、弹炮间距和相对弹道高 3个弹道环境信息的概念, 然后应用数学方法对弹目间距、弹炮间距和相对弹道高进行了理论计算推导, 建立了数学解算模型, 并用MATLAB程序进行了数值仿真计算, 通过分析其数值变化的规律和特点提出了其应用方向。     

装备科研招标项目的价值工程评标模型

应用价值工程分析方法系统研究装备科研招标项目的评标问题,提出了功能指标体系,建立了功能评价系数、成本评价系数和价值评价系数模型,并举例介绍了此评标方法的实现过程。     

舰艇设计中的生命力要求

生命力是舰艇设计中的一个重要因素.但是,由于缺少相应的标准评估方法、考核指标与定量设计约束要求,舰艇生命力一直未能很好地融入舰艇设计过程中.针对作战舰艇生命力设计优化,提出了一种“自顶向下”的树状生命力分解定义结构,并建立了相应的生命力评估的指标体系.同时,给出了任务相关的生命力指标设计定量要求与概率要求.     

航空发动机在超声速引射系统中的应用分析

航空发动机可以对空气增压,并且增加气流温度,理论上存在应用于超声速引射系统的可能。分析了气源对引射器性能的影响以及引气对航空发动机的影响,介绍了3种航空发动机在超声速引射系统中可能的布局方案。针对某领域内的排气参数要求,分别对3种布局方案进行了计算分析。计算结果表明,当上游气体压强为0.044×10⁵ Pa和0.029 3×10⁵ Pa时,通过合理选择发动机的布局以及工作参数,发动机可以直接将上游气体排出或者作为驱动气源应用于超声速引射系统。     

军事电子信息系统能力需求分析概述

军事电子信息系统现已发展成为支持信息化作战的核心系统,基于该系统与作战思想、方式之间紧密关联的特殊性,阐述了军事电子信息系统能力需求分析在信息系统需求工程中的重要地位和作用,分析了军事电子信息系统能力需求分析的基本内容,探讨了能力需求分析的实施过程,并进行了弹道导弹信息感知系统能力需求分析。通过对军事电子信息系统能力需求分析实施过程及其应用的研究,为军事电子信息系统能力需求工程提供借鉴。     

战时工程保障能力分析方法

结合战时工程保障的特点及对作战行动的影响,在对比分析多种能力分析方法的基础上,提出了采用定量仿真模型分析战时工程保障能力的方法,通过建立工程保障活动的过程模型,利用仿真运算结果定量分析工程保障任务的完成情况及其对作战行动的可能影响。应用实践表明,该方法操作性强,能够反映工程保障过程中的动态过程和外界影响,便于分析人员了解各项工程保障能力的强弱,能够用于指导分析人员优化工程保障任务。     

航空燃料冰点快速测定方法

冰点是表征航空燃料低温使用性能的重要指标。常规冰点测定方法操作步骤复杂,测定时间长,影响航空燃料质量检测效率。基于光散射原理,将温度传感和光电检测技术应用于航空燃料冰点测定,利用燃料结晶对光散射和透射的影响,实现航空燃料冰点快速测定。该方法操作简单快速,检测1个油样用时少于15 min,大幅提高了冰点检测效率;试样体积仅需2 mL,有利于试验环境保护;测定结果重复性好,与标准方法 GB/T2430—2008具有良好的相关性。