美军战术级指挥信息系统界面设计的发展及启示

战术级指挥信息系统(T-C4ISR系统)是指挥控制师或师以下部队遂行战术任务的信息平台.围绕T-C4ISR系统用户界面设计相关问题展开如下研究:通过智能化战争条件下T-C4ISR系统界面应具有的新特点引入,首先介绍了美军T-C4ISR系统界面设计理论的演变;结合美军RAPTOR系统,介绍了生态界面设计理论的主要内容和应用;分析了生态界面设计理论对我军T-C4ISR系统建设的一些启示,并展望了下一步可以开展的主要工作.     

网络信息体系弹性影响因素重要性评估方法

针对网络信息体系弹性影响因素重要性评估问题,提出了一种基于熵理论的群决策方法.在分析网络信息体系弹性作用过程的基础上,提炼了网络信息体系弹性影响因素;由熵权以及个体决策结果和群决策结果的偏差量,定义了专家的客观权重;提出了一种基于偏离度的权重调整算法,设计了网络信息体系弹性影响因素重要度等级映射方法,通过算例仿真验证了该评估方法的有效性和可行性.     

武器平台信息系统现场可更换单元划分方法

针对功能综合化发展背景下的综合模块化武器平台信息系统综合化程度高、功能复杂,不便于维修保障等问题,采用功能/硬件资源的模糊聚类、多重模糊有向图等方法进行武器平台信息系统LRU划分,划分了通用处理模块、信号处理模块、图形图像处理模块、网络交换模块和电源变换模块等LRU.通过项目应用表明,该方法可显著缩短现场可更换时间,提高武器平台信息系统维修保障能力和"通用化、系列化、组合化"水平.     

潜艇应急上浮机动不稳定性建模与仿真

为了避免潜艇在应急上浮过程中,由于较快的上浮速度以及较大的负攻角,水动力呈现强非线性,在横向流作用下潜艇可能产生过大的横倾角甚至失稳倾覆.基于艇体水流入射角和方向角定义下的潜艇非线性水动力描述形式及其试验结果,采用一种新形式的大攻角非稳态潜艇操纵运动仿真数学模型,对高压气吹除主压载水舱后潜艇应急上浮过程的运动状态进行预报.采用拉瓦尔喷管理论对高压气吹除主压载水舱的热力学过程进行建模,并将该过程计算得到潜艇所受的复杂激变力作为潜艇操纵运动仿真数学模型的控制输入,计算结果表明:相较于高压气吹除指数模型,采用的拉瓦尔喷管模型能更为真实地反映实艇高压气吹除过程,对潜艇应急上浮机动的运动状态预报更为准确.应急上浮过程中快速造成较大的尾倾角有利于抑制横倾角的增大,且横倾角主要受水舱吹除顺序的影响,受初始深度的影响较小.根据潜艇事故工况下的初始状态制定有效的高压气应急吹除挽回策略,是抑制应急上浮横倾角的主要手段.     

一种基于地表类型的地杂波快速仿真方法

地杂波仿真技术对机载雷达的设计与研制有着重要影响.针对机载雷达地杂波仿真技术开展研究,提出了一种基于地表类型的地杂波快速仿真方法.该方法以数字地图和载机航线为两个重要输入,采用雷达波束照射区域的数字地图为有效先验地理环境信息进行仿真,提高了杂波仿真的逼真度;同时针对传统仿真方法中计算量较大的问题,优化了散射单元中天线功率增益的计算方法,减少了仿真时间.对所提方法进行了计算机仿真验证,结果表明,该方法能够仿真多种场景下与实测数据高度近似的地杂波.     

Multi-objectives nonlinear structure optimization for actuator in trajectory correction fuze subject to high impact loadings

This paper presents an actuator used for the trajectory correction fuze, which is subject to high impact loadings during launch. A simulation method is carried out to obtain the peak-peak stress value of each component, from which the ball bearings are possible failures according to the results. Subsequently, three schemes against impact loadings, full-element deep groove ball bearing and integrated raceway, needle roller thrust bearing assembly, and gaskets are utilized for redesigning the actuator to effectively reduce the bearings' stress. However, multi-objectives optimization still needs to be conducted for the gaskets to decrease the stress value further to the yield stress. Four gasket's structure parameters and three bearings' peak-peak stress are served as the four optimization variables and three objectives, respectively. Optimized Latin hypercube design is used for generating sample points, and Kriging model selected according to estimation result can establish the relationship between the variables and objec-tives, representing the simulation which is time-consuming. Accordingly, two optimization algorithms work out the Pareto solutions, from which the best solutions are selected, and verified by the simulation to determine the gaskets optimized structure parameters. It can be concluded that the simulation and optimization method based on these components is effective and efficient.     

Study of high-speed-impact-induced conoidal fracture of Ti alloy layer in composite armor plate composed of Ti-and Al-alloy layers

In order to understand the mechanism of conoidal fracture damage caused by a high-speed fragment-simulating projectile in titanium alloy layer of a composite armor plate composed of titanium- and aluminum-alloy layers, the ballistic interaction process was successfully simulated based on the Tuler-Butcher and GISSMO coupling failure model. The simulated conoidal fracture morphology was in good agreement with the three-dimensional industrial-computed-tomography image. Further, three main damage zones (zones I, II, and III) were identified besides the crater area, which are located respectively near the crater area, at the back of the target plate, and directly below the crater area. Under the high-speed-impact conditions, in zone II, cracks began to form at the end of the period of crack formation in zone I, but crack formation in zone III started before the end of crack formation in zone II. Further, the damage mechanism differed for different stress states. The microcracks in zone I were formed both by void connection and shear deformation. In the formation of zone I, the stress triaxiality ranged from-2.0 to-1.0, and the shear failure mechanism played a dominant role. The microcracks in zone II showed the combined features of shear deformation and void connection, and during the for-mation process, the stress triaxiality was between 0 and 0.5 with a mixed failure mode. Further, the microcracks in zone III showed obvious characteristics of void connection caused by local melting. During the zone III formation, the triaxiality was 1.0-1.9, and the ductile fracture mechanism was dominant, which also reflects the phenomenon of spallation.     

Fuzzy recognition of missile borne multi-line array infrared detection based on size calculating

In order to improve the infrared detection and discrimination ability of the smart munition to the dy-namic armor target under the complex background, the multi-line array infrared detection system is established based on the combination of the single unit infrared detector. The surface dimension features of ground armored targets are identified by size calculating solution algorithm. The signal response value and the value of size calculating are identified by the method of fuzzy recognition to make the fuzzy classification judgment for armored target. According to the characteristics of the target signal, a custom threshold de-noising function is proposed to solve the problem of signal preprocessing. The multi-line array infrared detection can complete the scanning detection in a large area in a short time with the characteristics of smart munition in the steady-state scanning stage. The method solves the disadvan-tages of wide scanning interval and low detection probability of single unit infrared detection. By reducing the scanning interval, the number of random rendezvous in the infrared feature area of the upper surface is increased, the accuracy of the size calculating is guaranteed. The experiments results show that in the fuzzy recognition method, the size calculating is introduced as the feature operator, which can improve the recognition ability of the ground armor target with different shape size.     

武器装备体系贡献率研究现状分析

武器装备体系贡献率是全面、科学地评估武器装备在体系中发挥作用情况的指标,是目前装备论证领域的研究热点.收集了近年来国内在该领域的研究成果和国外与之相关的研究成果,通过对武器装备体系贡献率的概念内涵、属性特征、评估指标和方法的总结归纳,分析了研究中亟待解决的问题和面临的挑战,为武器装备体系贡献率的研究工作提供参考借鉴.     

Theoretical and numerical simulation study on jet formation and penetration of different liner structures driven by electromagnetic pressure

The use of a shaped liner driven by electromagnetic force is a new means of forming jets. To study the mechanism of jet formation driven by electromagnetic force, we considered the current skin effect and the characteristics of electromagnetic loading and established a coupling model of"Electric—Magnetic—Force"and the theoretical model of jet formation under electromagnetic force. The jet formation and penetration of conical and trumpet liners have been calculated. Then, a numerical simulation of liner collapse under electromagnetic force, jet generation, and the stretching motion were performed using an ANSYS multiphysics processor. The calculated jet velocity, jet shape, and depth of penetration were consistent with the experimental results, with a relative error of less than 10％. In addition, we calculated the jet formation of different curvature trumpet liners driven by the same loading condition and ob-tained the influence rule of the curvature of the liner on jet formation. Results show that the theoretical model and the ANSYS multiphysics numerical method can effectively calculate the jet formation of liners driven by electromagnetic force, and in a certain range, the greater the curvature of the liner is, the greater the jet velocity is.