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Relationships between Cyberspace Operations and Information Operations 网络空间作战与信息作战的关系
Q4 Engineering Pub Date : 2021-06-30 DOI: 10.3849/aimt.01466
Zsolt Haig
Today thanks to the wireless networking technologies and social networks, the inter-pretation of cyberspace has expanded. According to the three-layered structure of cyberspace, not only logical effects can be induced in this domain, e.g. by malwares, but physical and cognitive effects also appear in the physical and cyber-persona lay-ers, e.g. electronic jamming the wireless communications of network or influencing and manipulating users. This approach provides an opportunity to interpret cyberspace operations in a more complex way and to apply integrated technical and cognitive information capabilities that exploit each others effects. Accordingly, this study pre-sents an expanded interpretation of cyberspace, a novel and complex approach to cyberspace operations, as well as the information capabilities that can be used in these operations.
今天,由于无线网络技术和社交网络,网络空间的相互解释已经扩大。根据网络空间的三层结构,不仅可以在该领域引发逻辑效应,例如恶意软件,而且物理和认知效应也会出现在物理和网络人物身上,例如电子干扰网络的无线通信或影响和操纵用户。这种方法提供了一个机会,以更复杂的方式解释网络空间操作,并应用综合技术和认知信息能力,利用彼此的影响。因此,本研究对网络空间进行了扩展解释,提出了一种新颖而复杂的网络空间作战方法,以及可用于这些作战的信息能力。
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引用次数: 0
Improvement of Barrel Weapons Interior Ballistic Model Using Dynamic Vivacity Function 用动态活度函数改进炮管武器内弹道模型
Q4 Engineering Pub Date : 2021-06-30 DOI: 10.3849/aimt.01300
M. Schmidt, S. Beer, P. Konečný
The paper discuses a possibility of application of the dynamic vivacity function defined in COS 137604 (STANAG 4115) at the interior ballistic process mathematical model conversion. At present time various technologies of powder grain surfacing are used mainly in case of powders used in assemblies of small-calibre cartridges. The grain surfacing can properly influence the shot process, change character of the powder grain burning which cannot be described by the burning theory according to geometrical rules. COS 137604 determines necessity of the dynamic vivacity function L evaluation for artillery powders only, but the way of its evaluation can be applied for arbitrary powder. It then allows the get results of the interior ballistic tasks solutions with higher accuracy as well as the choice of the suitable grain surfacing technology.
本文讨论了COS 137604(STANAG 4115)中定义的动态活度函数在内弹道过程数学模型转换中的应用可能性。目前,各种粉末颗粒堆焊技术主要用于小口径弹药筒组件中使用的粉末。颗粒堆焊可以适当地影响喷丸过程,改变燃烧理论根据几何规律无法描述的粉末颗粒燃烧特性。COS 137604仅确定了火炮火药动态活度函数L评价的必要性,但其评价方法可适用于任意火药。然后,它可以获得更高精度的内弹道任务解决方案的结果,并可以选择合适的晶粒堆焊技术。
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引用次数: 0
Calculation Method Modification of Spare Parts Quan-tity to Restore Operability of Weapon Systems 修改备件数量以恢复武器系统可操作性的计算方法
Q4 Engineering Pub Date : 2021-06-30 DOI: 10.3849/aimt.01479
P. Openko, V. Mirnenko, V. V. Turin, M. Y. Myronuk, O. Doska, A. M. Bulay
The article proposes a methodical approach to calculating the number of spare parts for weapon systems (WS) combat damage elimination and operability restoration based on criteria of minimization of spare parts cost, meeting the requirements of the spare parts, tools, supplies and materials, as well as timeliness of damaged WSs repair. The main points of the methodological approach (mathematical formalization of the task, basic calculation ratios, stages and order of calculation of spare parts stocks) are represented with a simplified scheme of the calculation of spare parts to ensure WS combat damage elimination and operability restoration. Probability of sufficiency and developed mathematical model for its calculation are used as a sufficiency indicator of spare parts to ensure WS combat damage elimination and operability restoration.
本文提出了一种基于备件成本最小化、满足备件、工具、用品和材料要求以及受损武器系统维修及时性的标准,系统地计算武器系统作战损伤消除和可操作性恢复备件数量的方法。方法论方法的要点(任务的数学形式化、基本计算比率、备件库存计算的阶段和顺序)用备件计算的简化方案来表示,以确保消除WS作战损伤和恢复可操作性。将备件的充足率及其计算数学模型作为备件的充足性指标,以确保WS作战损伤的消除和可操作性的恢复。
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引用次数: 3
Dynamic Simulation Analysis and Optimization of Firing Rate of Rocket Launchers on Wheeled Vehicles 轮式运载火箭发射装置射速的动态仿真分析与优化
Q4 Engineering Pub Date : 2021-06-30 DOI: 10.3849/aimt.01459
Vo van Bien, Martin Macko, N. Dung, Nguyen Duy Phon, N. Hai, Bui Trong Tuan
The paper presents a method of determining the dynamic parameters of multiple-rocket-launcher system mounted on the wheeled vehicle based on Newton's law of motion. The dynamic simulation was conducted and then the results were compared with the corre-sponding experimental data to verify the reliability of the model. The model was ap-plied in calculation and tested out on multiple-rocket-launcher system B?-21 (of Rus-sia). The theoretical model calculation results are relatively consistent with the meas-ured experimental data. The dependence of the launcher oscillation on the rate of fire was investigated, which determined the optimal rate of fire for each launcher. These results are used to evaluate the firing stability of the launcher when firing individual shots and firing bursts. This is an important theoretical basis which can be a reference for designers in the design process of improvement, manufacture, exploitation and use of a launcher mounted on the wheeled vehicle.
本文提出了一种基于牛顿运动定律确定轮式运载火箭多管火箭炮系统动力学参数的方法。进行了动力学仿真,并将仿真结果与相应的实验数据进行了比较,验证了模型的可靠性。该模型在多管火箭炮系统B-21(俄罗斯)。理论模型计算结果与实测实验数据比较一致。研究了发射器振荡对射速的依赖性,从而确定了每个发射器的最佳射速。这些结果用于评估发射装置在单独发射和发射突发时的发射稳定性。这是一个重要的理论基础,可供设计人员在轮式车辆发射装置的改进、制造、开发和使用的设计过程中参考。
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引用次数: 2
An Efficient Destructive Interference Based on Side Lobe Suppression Method in SONAR Beamforming SONAR波束形成中一种有效的基于旁瓣抑制的破坏性干扰方法
Q4 Engineering Pub Date : 2021-06-30 DOI: 10.3849/aimt.01429
S. Pillai, T. Santhanakrishnan, R. Rajesh
A novel beamforming technique that resembles the principle of interference is proposed for sonar arrays to suppress the side lobes while the main lobe is kept intact. It uses two window functions. The first one is a rectangular function that produces a primary beam pattern. A secondary new window function is derived and its beam pattern is steered such that the null or trough of the main lobe of the new window coincides with the peak or crest of the first side lobe of the rectangular window and so on to other major side lobes. Pattern multiplication was used to get a final beam pattern. The approach is simulated and verified through a sonar array with 24 hydrophone sensors.
提出了一种新的波束形成技术,该技术类似于干扰原理,用于声纳阵列抑制旁瓣,同时保持主瓣不变。它使用两个窗口函数。第一个是一个矩形函数,它产生一个主光束模式。导出次级新窗口函数,并操纵其波束方向图,使得新窗口的主瓣的零点或波谷与矩形窗口的第一旁瓣的峰值或波峰重合,以此类推。图案相乘用于获得最终的光束图案。该方法通过一个带有24个水听器传感器的声纳阵列进行了仿真和验证。
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引用次数: 4
Runway Excursions: Bearing Strength Control of Unpaved Areas 跑道偏移:未铺砌区域的承载强度控制
Q4 Engineering Pub Date : 2021-06-30 DOI: 10.3849/aimt.01432
Ludek Cicmanec, Ondřej Ulrich
The paper deals with the Dynamic Cone Penetrometer application which is intended to work as a vital means to support the bearing strength evaluation over the vast unpaved airport areas. Having identified fundamental drawbacks, the authors proposed some refinements in the original methodology. These predominantly respect the needs of airport operation services. Specifically, the model based on fuzzy logic and two tables, exceptionally suitable for day-to-day applications, are proposed and tested upon the extensive data set acquired at four airports over the last four years.
本文介绍了动态圆锥贯入仪的应用,该仪器旨在作为一种重要手段,支持在广阔的未铺砌机场区域进行承载强度评估。在发现了根本缺陷后,作者提出了对原始方法的一些改进。这些主要是为了满足机场运营服务的需要。具体而言,提出了基于模糊逻辑和两个表的模型,特别适合日常应用,并在过去四年中在四个机场获得的大量数据集上进行了测试。
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引用次数: 0
A Helmet Cueing System Based Firing Controlfor Anti-Aircraft Gun Prototype 基于头盔提示系统的高炮原型射击控制
Q4 Engineering Pub Date : 2021-06-30 DOI: 10.3849/aimt.01364
S. Mekonnen, M. Asrat, S. Ramasamy
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引用次数: 2
Evolution from the Network-Centric Warfare Сoncept to the Data-Centric Operation Theory 从网络中心战概念到数据中心作战理论的演进
Q4 Engineering Pub Date : 2021-06-21 DOI: 10.3849/aimt.1430
A. Skoryk, Boris Nizienko, A. Dudush, V. Shulezhko, Irina Romanchenko
The article analyzes the impact of disruptive technologies on the evolutionary development of military architectural frameworks and concepts of warfare. It argues the need for a transition from the Network-Centric Warfare concept to the Data-Centric Operation theory and proposes a 4D-extensional representation of the combat space of weapon systems integrated into a single network. It is concluded that there is hardware redundancy in modern weapon systems and it is possible to use it as a network resource, the management of which provides additional opportunities for improving operational capabilities.
本文分析了颠覆性技术对军事架构框架和战争概念演化发展的影响。它论证了从网络中心战概念向数据中心作战理论过渡的必要性,并提出了集成到单个网络中的武器系统作战空间的4d扩展表示。结论是,在现代武器系统中存在硬件冗余,并且有可能将其用作网络资源,其管理为改进作战能力提供了额外的机会。
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引用次数: 1
Numerical Analysis of the Ability of a Floating Vehicle to Overcome a Water Obstacle 浮式车辆克服水障能力的数值分析
Q4 Engineering Pub Date : 2021-06-08 DOI: 10.3849/aimt.01476
K. Kosiuczenko, R. Sosnowicz
The paper presents the results of simulation tests of the entry of a floating transporter to a water obstacle. The simulation tests were performed with the use of LS Dyna program, based on the finite element method (FEM). The computational model was developed and used in the simulation of the manoeuvre of entering the water obstacle for the extreme conditions, which are described by NATO standards. For a model, as an example vehicle, the floating transporter PTS-M was used. The results of the application of the elaborated model confirmed the possibility to utilise the method to verify the behaviour of a vehicle in a very important and difficult problem from the point of view of vehicle safety conditions.
本文介绍了浮式输送机进入水障的模拟试验结果。基于有限元法,利用LS Dyna程序进行了模拟试验。建立了该计算模型,并将其应用于北约标准所描述的极端条件下的水障机动模拟。对于一个模型,作为一个例子车辆,浮动运输车PTS-M被使用。详细模型的应用结果证实了利用该方法从车辆安全条件的角度验证车辆在一个非常重要和困难的问题中的行为的可能性。
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引用次数: 1
Effect of some Disturbance Factors on Falling Point Distribution of Unguided Rocket 干扰因素对非制导火箭落点分布的影响
Q4 Engineering Pub Date : 2021-05-16 DOI: 10.3849/aimt.1446
Huu Le Ban, P. Konečný
The paper investigates the individual and combined effects of disturbance factors including thrust misalignment, the offset of the centre of gravity and misalignment of the principal axes of inertia on falling point distribution of a type of unguided rocket (fin-stabilized rockets with single-stage solid-propellant rocket engines). The mathematical model used in the paper is developed from an available rocket motion model and solved for a representative rocket which is BM-21 rocket. The obtained results show dependencies of falling point deviation on disturbance parameters. These dependencies agree with the standard data given in the firing table; in addition, they are fuller and more insight ful than the previous research.
研究了推力偏差、重心偏移和惯性主轴偏差等干扰因素对某型无制导火箭(单级固体火箭发动机翅片稳定火箭)落点分布的单独和综合影响。本文所用的数学模型是在现有火箭运动模型的基础上发展起来的,并针对具有代表性的BM-21火箭进行了求解。结果表明,下降点偏差与扰动参数之间存在相关性。这些依赖关系与激发表中给出的标准数据一致;此外,它们比以前的研究更全面、更有洞察力。
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引用次数: 3
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Advances in Military Technology
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