数字化部队装备维修保障业务流程再造研究

将业务流程再造的思想应用到数字化部队装备保障中,分析数字化部队装备保障业务流程再造的基础,阐述了再造过程中信息技术的运用要求,提出了再造的步骤,最后通过对现有装备修理业务流程的分析,对数字化部队修理业务流程进行了再造的设计构想。     

AHP-Fuzzy法评估C4ISR系统作战效能中的应用

C4ISR系统在现代战争中的重要作用使得其评价问题得到了前所未有的重视.结合C4ISR系统的实战情况,通过对影响其作战效能不确定因素的分析和处理,运用AHP-Fuzzy分析法,建立了C4ISR系统作战效能的综合量化评估模型,讨论了联合作战中C4ISR系统的定量评估方法.最后通过算例,证明了此方法的有效性和可行性,为C4ISR系统的效能评估提供了一种有效的方法和途径.     

【专题】运用时空大数据增强战场态势感知能力

时空数据是同时具有时间、空间和专题属性的三维数据。近年来,时空大数据技术领域取得重大进展,时空大数据也开始逐渐应用于战场态势感知,辅助联合作战指挥决策,推动了智能化战争的快速演进。本文基于未来战场对一体化联合作战战场态势感知的新要求,从用于支撑战场态势感知的时空大数据平台构建、时空大数据来源拓展和平台的优化利用等三个层次,探讨了打造军事作战资源“一张图”以支撑一体化联合作战战场态势感知的可行性;同时,对时空数据结构、数据平台和数据分析计算方法等方面进行了深入分析和重点布局。研究成果可对解决“参战力量在哪里,可配合的友邻力量有哪些,能使用的军事资源有什么”等问题和提升基于时空大数据技术的联合作战、全域作战能力提供技术及理论支撑。     

基于时间分布函数的武警指挥速度评估模型

指挥速度是武警指战员筹划和组织指挥处置行动的基本依据,对保证指挥流程高效有序运行具有十分重要的作用.通过分析指挥流程传统认识上的不足,运用系统论对指挥流程进行更完善的描述,指出在相同工作量下,影响指挥流程的核心因素是流程运行中指挥速度的时间,运用概率统计方法将流程持续时间确定为服从Be-ta-PERT分布函数,建立了基于时间分布函数的指挥速度评估模型,详细阐述了模型的求解过程,并提出了该模型在实际中的应用策略.     

多波束干扰系统多目标干扰决策研究

针对多波束地对空雷达干扰系统同时干扰多目标的资源分配问题,为充分利用干扰资源,综合考虑个体干扰有效与整体干扰效益最大.基于目标威胁等级,围绕发现概率下降程度、定位误差增大程度、干扰有效率3个评估指标,建立多目标优化分配模型,对阵面资源进行动态分配,并利用非支配排序遗传算法进行仿真验证.仿真结果表明,该分配模型可充分发挥多波束干扰系统的优势,实现不同作战阶段干扰效益最大化.     

Fabrication and analysis of TIG welding-brazing butt joints of in-situ TiB2/7050 composite and TA2

Lightweight hybrid structures of Al MMCs and titanium alloy dissimilar materials have great prospect in the defence industry application. So, it is necessary to join Al MMCs with Ti metal to achieve this structural design. In this work, in-situ TiB2/7050 composite and TA2 were firstly attempted to join by TIG welding-brazing technique. The result was that the intact welding-brazing butt joint was successfully fabricated. The joint presents dual characteristics, being a brazing on TA2 side and a welding on TiB2/7050 side. At brazing joint side, ER4043 filler metal effectively wets on TA2 under TIG heating condition, and a continuous interfacial reaction layer with 1—3μm is formed at welded metal/TA2 interface. The whole interfacial reaction layers are composed of Ti(AlSi)3 intermetallic compounds (IMCs), but their morphologies at the different regions present obvious distinguishes. The microhardness of the reaction layers is as much as 141—190 HV. At welding joints side, the fusion zone appears the equixaed crystal structure, and the grain sizes are much smaller than those of welded metal, which is attributed to the effect of TiB2 particulates from the melted TiB2/7050 on acceleration formation and inhibiting growth for the new crystal nucleus. The tensile test results show that average tensile strength of the optimal welding-brazing joint is able to achieve 138 MPa. The failure of the tensile joint occurs by quasi-cleavage pattern, and the cracks initiate from the IMCs layer at the groove surface of TA2 and propagate into the welded metal.     

Research on the intermediate phase of 40CrMnSiB steel shell under different heat treatments

In this study, 40CrMnSiB steel cylindrical shells were tempered at 350, 500 and 600 ℃ to study the effect of tempering temperature on the dynamic process of expansion and fracture of the metal shell. A mid-explosion recovery experiment for the metal cylinder under internal explosive loading was designed, and the wreckage of the casings at the intermediate phase was obtained. The effects of different tempering temperatures on the macroscopic and microscopic fracture characteristics of 40CrMnSiB steel were studied. The influence of tempering temperatures on the fracture characteristic parameters of the recovered wreckage were measured and analyzed, including the circumferential divide size, the thick-ness and the number of the circumferential divisions. The results show that as the tempering temper-ature was increased from 350 to 600 ℃, at first, the degree of fragmentation and the fracture characteristic parameters of the recovered wreckage changed significantly and then became essentially consistent. Scanning electron microscopy analysis revealed flow-like structure characteristics caused by adiabatic shear on different fracture surfaces. At the detonation initiation end of the casing, fracturing was formed by tearing along the crack, which existed a distance from the initiation end and propagated along the axis direction. In contrast, the fracturing near the middle position consists of a plurality of radial shear fracture units. The amount of alloy carbide that was precipitated during the tempering process increased continuously with tempering temperature, leading to an increasing number of spherical carbide particles scattered around the fracture surface.     

Thermal and combustion behavior of Al-MnO2 nanothermite with poly(vinylidene fluoride -co- hexafluoropropylene) energetic binder

Fluoropolymers get increasing attention in energetic materials application due to the high fluorine content. To explore the effect of poly(vinylidene fluoride-co-hexafluoropropylene) (P(VDF-HFP)) on Al/MnO2 nanothermite, the samples with different contents are prepared and characterized by SEM, TG-DSC, XRD, and their ignition and combustion behavior are tested and recorded. The results show that P(VDF-HFP) as an energetic binder can combine the nanothermite components together, even exist in the gaps. The integrity of energetic materials has been improved. Thermal analysis shows that the addition of P(VDF-HFP) greatly changes the thermal reaction processes, and the exothermic peaks appear early, but the utilization of fuel and oxidizer is not efficient from the XRD results. Furthermore, the appropriate addition of P(VDF-HFP) can directly reduce the ignition energy threshold and increase the combustion time, which is necessary for the potential ignition charge application. The possible reasons for above phenomena are discussed and analyzed. This research provides a reference for improvement of thermite-based ignition charge formulation.     

Finite-time tracking control and vibration suppression based on the concept of virtual control force for flexible two-link space robot

The dynamic modeling, finite-time trajectory tracking control and vibration suppression of a flexible two-link space robot are studied. Firstly, the dynamic model of the system is established by combining Lagrange method with assumed mode method. In order to ensure that the base attitude and the joints of space robot can reach the desired positions within a limited time, a non-singular fast terminal sliding mode (NFTSM) controller is designed, which realizes the finite-time convergence of the trajectory tracking errors. Subsequently, for the sake of suppressing the vibrations of flexible links, a hybrid tra-jectory based on the concept of the virtual control force is developed, which can reflect the flexible modes and the trajectory tracking errors simultaneously. By modifying the original control scheme, a NFTSM hybrid controller is proposed. The hybrid control scheme can not only realized attitude stabili-zation and trajectory tracking of joints in finite time, but also provide a new method of vibration sup-pression. The simulation results verify the effectiveness of the designed hybrid control strategy.     

Barrier Lyapunov functions-based dynamic surface control with tracking error constraints for ammunition manipulator electro-hydraulic system

This paper focuses on the dynamic tracking control of ammunition manipulator system. A standard state space model for the ammunition manipulator electro-hydraulic system (AMEHS) with inherent non-linearities and uncertainties considered was established. To simultaneously suppress the violation of tracking error constraints and the complexity of differential explosion, a barrier Lyapunov functions-based dynamic surface control (BLF-DSC) method was proposed for the position tracking control of the ammunition manipulator. Theoretical analysis prove the stability of the closed-loop overall system and the tracking error converges to a prescribed neighborhood asymptotically. The effectiveness and dynamic tracking performance of the proposed control strategy is validated via simulation and experi-mental results.