根据输入噪声估算通信距离

提出并论证了一种根据输入噪声估算战术电台通信距离的方法,并且以VRC-8000电台在城郊通信为例进行了具体的分析计算.该方法对于实现战术电台迅速、可靠地通信有实际意义.本文进而提出了检测电台收信机输入噪声的技术方案,供选用.     

相控阵技术在无人机"一站多机"方案中的应用

研究了相控阵技术的基本特点及其实现多目标跟踪与测控的基本原理 ,分析了基于相控阵技术的“一站控制多机”的实现技术 ,给出了一种实现方案 ,并探讨了其可行性     

隐身飞机RCS测量与成像方法研究综述

隐身飞机已逐步成为大国重器,并将持续发挥重要影响,隐身技术也已成为飞行器设计的关键技术。隐身飞机的雷达散射截面积(radar cross section, RCS)测量是设计、制造、维护隐身飞机的必要手段。从缩比模型的RCS测试、全尺寸飞机室外RCS测试、全尺寸飞机室内近场测试三个方面,回顾了隐身飞机RCS测量的基本流程,总结了隐身飞机RCS近场测量的理论基础,并着重对具有成像诊断功能的近场RCS测量技术进行了梳理与分析。对隐身飞机RCS测量的应用趋势和关键技术进行了总结与展望, 有利于对隐身飞机RCS测量形成总体性了解,并把握RCS测量的发展方向。     

Operating Costs of Aging Air Force Aircraft: Adjusting for Aggregate Budget Effects

The rate at which operating costs grow as aircraft age is important for setting operating budgets and for deciding when to replace aging systems. While studies using data from the 1990's typically found 1–3 percent real rates of growth in operating costs as aircraft age, studies using data from the 2000's found greater rates, for example in the 4–6 percent range. Growth in the total U.S. Air Force budget during the 2000s appears to explain much of the higher estimated annual growth rates in operating costs per flying hour beyond the growth rate intrinsic to the aging of the fleet.     

Fighter aircraft acquisition in Croatia: failure of policy delivery

The possibility for Croatia to obtain new fighter aircraft is not new, as this option has been publicly debated for at least a decade. A sudden decision to advance the acquisition of a limited number of fighter aircraft was made in 2017 with an international tendering process concluding in early 2018. Through open source material, this paper will look at this procurement process by examining the relationship between policy and strategic thinking on the one side, and policy delivery on the other, and evaluate why the tendering process failed in achieving envisaged results. The paper concludes that the problems facing the Croatian aircraft acquisition process stem from at least two interrelated factors: firstly, at the operational level, the failure of the procurement was the direct result of mismanaged tendering procedures linked to the wider public administration reform process; and secondly, at the strategic level, inherently complex civil-military relations and related cultural aspects which have not been adequately addressed over the past decades. The result was a failure to deliver on government policy, something which this paper argues will need to be addressed over the medium to long term.     

目次

为改善等离子体合成射流激励器在稀薄空气环境中的控制效果,增强其临近空间环境适应性,开展了腔体增压条件下激励器工作特性的研究。建立了腔体增压效果理论分析模型,计算结果表明:采用高压气源供气可以较好地提升激励器腔体气压,并且腔体气压对高压气源气压具有较好的跟随性,从而为射流强度调节提供了一种新的方式。搭建了腔体增压等离子体合成射流激励器实验系统,开展了腔体增压压力和射流流场特性测量,实验测量结果与计算结果吻合良好,误差小于2.6%。高速纹影观测显示:在腔体增压作用下,激励器控制力得到显著改善,射流锋面峰值速度由256 m/s提升至507 m/s。     

基于系统构型替换的固冲发动机故障模式半实物仿真

为全面快速验证冲压发动机的故障检测算法,基于构型替换建立了能模拟多种固冲发动机故障的仿真验证平台。基于此平台,搭建了发动机点火故障模型、压强传感器故障模型、设备接口模型,以及与真实控制器中检测算法具有相同外部接口和系统构型的故障检测算法模型等。通过系统构型的切换,将同一个故障模式注入故障检测算法模型和真实发动机系统,并通过对比同一组故障模式下故障检测模型检测结果与发动机控制系统检测结果,来对发动机控制器中的故障检测算法进行快速验证。以无喷管助推器点火的检测为例,讲述了该方法的建模、实验验证及分析过程,此外,该方法还能应用到无喷管助推器关机、进气道前后堵盖打开、燃气发生器点火、燃气流量容错控制等多个故障模式的仿真模拟与验证,具有很强的通用性,能大大地降低控制系统开发与验证的时间成本,具有很强的应用价值。     

美军战术车辆作战试验现状分析

以美军战术车辆为研究对象,介绍了美军战术车辆的基本概况,分析了美军战术车辆作战试验类型,系统研究了美军轻型、中型、重型战术车辆及防地雷反伏击车的作战试验现状和特点,提出了对我军开展战术车辆作战试验的启示。     

高超声速变形飞行器翼面变形模式分析

为提高高超声速翼身组合式飞行器的射程,研究了采用不同翼面变形模式时,飞行器在马赫数3~8内的气动特性和翼面效率。针对典型的轴对称翼身组合式外形,采用Navier-Stokes方程进行数值模拟,对伸缩、变后掠和二维折叠三种变形模式下的外形在超声速及高超声速来流条件下进行模拟,并对升阻比、翼面单位面积升阻比和操稳特性进行分析。结果表明:在超声速及高超声速范围内,变后掠变形模式在宽速域内升阻比提高明显,同时具备优良的翼面效率及操稳特性,其在马赫数3~8范围内具有最优的综合性能。研究成果能对高超声速翼身组合式变形飞行器布局设计提供参考,具有一定的指导意义。     

舰载机轮胎子午化可行性研究

文章以制约我国舰载机发展的关键技术航空轮胎为着眼点,通过研究国内外舰载机轮胎发展现状,对舰载机轮胎子午化的可行性进行了分析,提出了舰载机轮胎子午化势在必行的论断,为新研制的各型舰载机项目提供有力支持。