船舶柴油机轴系有阻尼强迫扭振计算的扩展霍尔茨法

从力学原理的角度阐述了扩展霍尔茨法的理论基础,从而论证了其合理性．依据有关文献资料进一步完善了扩展霍尔茨法,使之适合于船舶工程界对强迫扭振计算不断提高的要求．提出了适于数值计算和易于编程的计算方法,并编制了相应的计算程序．实例计算及比较分析表明,该方法是适用的,可以用于船舶轴系的设计及强迫扭转振动计算．     

加农炮身管纵向振动的固有特征分析

建立了加农炮身管纵向振动的力学模型,推导出了频率方程,给出了固有频率的数值计算结果,描绘了加农炮身管纵向振动的固有振型,对影响加农炮身管纵向振动固有特征的各种因素进行了分析。     

磁悬浮隔振系统的行为与分析

磁悬浮隔振是一种新型的主动式隔振技术。文中首先对磁悬浮隔振系统做一般性的说明,然后以自行研制的磁悬浮隔振试验装置为对象,分析了磁悬浮隔振的机理和特性;论述了磁悬浮隔振系统的建模和控制策略;最后对磁悬浮隔振系统运行与特性进行分析并给出了分析结果和仿真结果的比较。     

飞行计划管理中航迹关联算法

针对传统飞行计划管理中的缺限,基于MK-NN航迹关联算法思想,提出了一种利用方向因子、速度因子、偏航因子、时差因子和区域因子对综合航迹和计划航迹进行比较关联的方法.通过仿真,分析比较了该算法与其它算法的综合性能,验证了MK-NN算法在计划管理中的科学性和可行性.用改进的MK-NN算法为基本算法实现对飞行计划实施的动态监控,能够提高飞行计划管理的准确性和可靠性.     

一种以太网系统监控的双独立互联系统

针对现有技术对高可靠性以太网系统进行监控,具有明显的缺陷和不足之处.提出了一种由用户以太网系统和附加的平衡结构外,总线互连系统组成以太网监控的双独立互连系统.在分析了该系统结构和工作原理的基础上,对系统的可靠度和可用度进行分析计算,为系统的实现提供了重要的依据.     

Novel approach for active vibration control of a flexible missile

This paper investigates the feasibility of using an active dynamic vibration absorber (ADVA) for active vibration control of a flexible missile system through simulation. Based on the principles of a dynamic vibration absorber (DVA), a ring-type ADVA is first designed to attenuate the elastic vibration of the flexible missile, and the design of the active controller adopts the proportional-integral-derivative (PID) control algorithm. The motion equations of a flexible missile with an ADVA, which is subjected to follower thrust at its aft end, are derived using the Lagrangian approach. Taking the minimum of the root mean square (RMS) of the lateral displacement response of the center of mass as the objective function, a genetic algorithm (GA) is used to optimize the parameter of the DVA and PID controller. The numerical calculations show that the ADVA and DVA are effective in suppressing the vibration and provide approximately 41.2% and 17.6% improvement, respectively, compared with the case of no DVA. The ADVA has better performance than the DVA. When the missile is subjected to follower thrust, the effect of vibration reduction is more effective than the case without follower thrust. It is feasible to reduce vibration and improve the stability of flexible missiles by means of the ADVA.     

Combating nuclear smuggling? Exploring drivers and challenges to detecting nuclear and radiological materials at maritime facilities

International concern over nuclear terrorism has grown during the past few decades. This has driven a broad spectrum of efforts to strengthen nuclear security globally, including the widespread adoption of radiation-detection technology for border monitoring. Detection systems are now deployed at strategic locations for the purported purpose of detecting and deterring the smuggling of nuclear and radioactive materials. However, despite considerable investment in this area, few studies have examined how these programs are implemented or the operational challenges they face on a day-to-day basis. This article seeks to address this with a focus on radiation-detection efforts at maritime facilities. Utilizing practitioner interviews and a survey, this article identifies the factors that influence the planning and use of these systems in this fast-moving environment. The results clearly demonstrate that the implementation of these systems varies significantly across different national and organizational contexts, resulting in a fragmented global nuclear-detection architecture, which arguably undermines efforts to detect trafficked nuclear-threat materials. Greater consideration should therefore be given to developing international standards and guidance, designing and adopting tools to support key parts of the alarm assessment process, and broader sharing of good practice.     

电磁轨道发射中内弹道动力响应特性分析

将轨道简化为移动载荷作用下固定在弹性支撑上的Bernoulli-Euler梁,通过静态电磁-结构耦合有限元模型求得外围封装的等效刚度,计算得到发射器的临界速度。另外,利用混合有限元/边界元法建立电磁-结构-运动多物理场耦合的动力学模型,求得枢轨动态接触压力和轨道的应力应变分布特性。通过在轨道背面布置光纤光栅应变传感器,利用测量数据验证了动力响应特性,并分析了弹丸在内弹道的稳定性。针对典型30 mm × 30 mm矩形口径发射器,分析及试验结果表明：C型电枢对轨道的电磁挤压力在平顶沿起始时刻达到最大值,之后随着时间推移逐渐减小;电枢通过引起的应力波在高速段容易与轨道中反射应力波发生共振,并且轨道在电枢运动的中间高速段区域受力最为集中,应力集中水平约是起始低速段区域的2.44倍;电枢运动高速段会出现晃动现象,进而引起上下轨道受力的不对称性。分析及试验结果对研究电磁轨道发射器内弹道动力响应特性和发射器结构设计具有重要指导意义。     

基于动态行为监测的木马检测系统设计

首先介绍了特洛伊木马的基本概念及常用的木马检测方法,然后在分析传统的基于静态特征的木马检测技术缺点的基础上,结合基于动态行为监测的木马检测思想,研究以木马植入、隐蔽和恶意操作所需资源的控制和动态可疑行为监测相结合的隐藏木马检测技术,并提出了基于动态行为监测的木马检测系统的基本框架,给出了动态行为监测的相关策略和可疑行为的分析与判定的方法。     

两种捆绑火箭弹性振动建模方法对比分析及其对姿控系统的影响

针对长助推和短助推两种类型捆绑火箭的不同模态特点,分析了两者弹性振动建模方法的区别和联系,在此基础上建立了某型固体捆绑火箭姿态动力学新模型,模型中基于有限元法导出了弹性振动方程,基于该模型对箭体复杂弹性振动引起的通道间耦合进行了研究,采用逆Nyquist阵列法进行设计。结果表明,该模型能更准确地反映捆绑火箭纵、横、扭耦合运动特性;新模型三通道之间存在弹性耦合,但耦合矩阵具有对角优势性质,采用逆Nyquist阵列法进行姿控系统设计是有效的,仿真结果表明设计的控制器可行,能够取得比较好的性能。