火炮身管寿命的分布函数

本文运用可靠性理论和《130mm 加农炮剩余寿命的一种预测模型》一文的结果,证明火炮身管寿命服从 Weibull 分布,并以130mm 加农炮为实例,给出参数的比值估计方法.     

干扰信号的软件处理方法

在测量过程中,干扰信号直接影响测量精度。本文讨论三种干扰信号分别造成的系统误差、随机误差以及粗大误差的软件处理方法,并给出了相应算法和处理流程。     

油料保障力评估方案中的兼容度运用研究

旨在寻求一种从众多备选油料保障力评估方案中产生优化方案的方法,引入 兼容度的概念,并建立了兼容度极大化模型,根据模型建立了油料保障力评估方案优化系 统。利用优化系统对6个部队的油料保障力评估过程中的4个评估方案进行优化,通过计 算、比较、择优,得到了最优评估方案。应用表明运用兼容度优化油料保障力评估方案是合 理和正确的。     

舰舰导弹武器系统作战效能评估

在规定舰舰导弹典型作战任务剖面的情况下,运用美国工业武器系统效能咨询委员会评估武器系统效能的方法,建立舰舰导弹武器系统作战效能评估数学模型,并进行了算例验证和分析。结果表明:该模型可有效评估舰舰导弹武器系统作战效能,为舰舰导弹武器系统作战效能的评估提供了有效且便于操作的方法。     

一种适用于长基线的改进CIR算法

长基线下,受伪距多径和电离层残差影响,传统的CIR法解算载波相位宽巷模糊度时某些历元无法得到正确的结果,基础载波模糊度的搜索范围也较大。分析了CIR法的模糊度误差,提出了基于载波相位平滑伪距并且消除电离层时延的改进的CIR算法,分析了其误差方差,最后利用Compass系统实测数据对短基线和长基线两种情况下CIR法和改进CIR法的解算结果进行比较。实测数据表明,本文提出的算法能够单历元解算超宽巷模糊度和宽巷模糊度,并且能够大大缩小基础载波模糊度的搜索空间。     

To Be or Not To Be: The Development of Soviet Deck Aviation

Few issues were as contentious in the development of the Soviet Navy as the role of aircraft carriers and sea-based aviation. Despite the continued insistence by the highest naval authorities and scientific experts that surface combatants simply could not be protected in the open ocean without the support of ship-borne aviation, Soviet leaders – for a variety of reasons – resisted aircraft carrier development until the final decades of the Cold War. In examining one of the most defining and telling asymmetries of the Cold War at sea, the author argues that while the USSR was economically and technologically capable of building aircraft carriers of any class, bureaucratic infighting, misperceptions of cost and practicality, and the inherent flaws of a totalitarian system ultimately created an impossible gap in capabilities between the two sides. The priorities and direction of Soviet weapons and defense technology development during the Cold War was largely a factor of the military-political situation taking shape at home, and in the world. As a rule, the navy was assigned missions that corresponded to its capabilities at a given point in time, rather than the other way around. Often, the navy lacked the material resources needed to implement its core mission. The availability of these resources, in turn, depended on the country's economic situation, its scientific potential, the technological state of its industry, as well as the subjective influence of political and military leaders on the priorities of technological development. The impact of the country's socioeconomic imperatives was undoubtedly also felt in the sluggish pace of development of ship-borne aviation and aircraft carriers in the USSR.     

装药长径比对EFP成型作用效果影响分析

针对装药长径比对EFP成型的影响,基于一种球缺型药型罩EFP,利用ANSYS／LS-DYNA仿真软件对其成型过程进行建模仿真,研究EFP成型过程及其各项参数．在该基础上,改变装药高度得到不同的装药长径比数据,并对不同长径比EFP形成过程进行仿真,得到不同装药长径比EFP的速度、速度增长率及炸药能量利用率等数据,为选择最佳装药长径比提供依据．     

基本作战样式下航母编队兵力配置方法

航母编队兵力配置是航母编队作战运用的基础内容,从作战任务的角度来研究航母编队兵力配置问题。航母编队基本作战样式可分为对空作战、对海作战、对潜作战和对岸作战4种,航母编队通过基本作战样式的组合来达成作战任务。基于每种作战样式下航母编队兵力执行的作战任务,确定了兵力配置的原则和方法。为研究航母编队兵力配置问题提供了一种可借鉴的思路。     

The defence firm of the future

This paper offers the personal view of a senior executive in the Defence Procurement Agency about the future requirements of the defence industry’s principal UK customer. The focus here is on trying to identify the type of corporate behaviour and range of skill sets that the UK Government will need from defence suppliers, both primes and supply chain companies in the future. The concluding message from this ‘Customer View’ is that there is likely to be a continuing market for the company that specializes in delivering defence capability. It will be a company that will be looking for a long‐term relationship, with a specialist knowledge of its various national customers and a willingness to work openly and closely with them. It will be agile in its ability to bring together diverse technologies, to package them as a system and to deliver them either as hardware or as a service. Such suppliers will also need to innovate and to adapt at least as rapidly as the threats that they seek to counter.     

高超声速飞行器分离干扰的伴随方法分析

以大气层内高超声速飞行器级间分离过程为研究对象,采用伴随方法得到了由冲击力和气动干扰力矩引起的攻角的解析解。利用该解析解,得到了分离干扰引起的攻角的瞬时变化曲线。结果表明,在高超声速飞行器级间分离开始0.4s内,冲击力和气动干扰力矩对攻角有一定的影响,并且随干扰的增大而增大。本研究实现了预示高超声速飞行器分离过程风险的目的,对高超声速飞行器分离干扰策略的制定提供了理论依据。