【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。     

高速SpaceFibre总线节点的系统设计

为了实现SpaceFibre总线节点的高效数据传输,针对网络协议中关键问题和技术提出了一种基于现场可编程门阵列(Field Programmable Gate Array,FPGA)的SpaceFibre总线节点系统设计方案。其中,采用了轮询仲裁算法,解决了多路虚拟通道中流量控制字的申请冲突;设计了基于服务质量机制的高效处理状态机,实现了多路虚拟通道的服务质量调度;提出了一种并行的分区存储架构和重发控制算法,实现了基于错误检测隔离恢复机制的错误恢复;采用了不同的数据并行处理方案,实现了多种数据格式的循环冗余校验和伪随机序列的计算。通过ModelSim仿真平台对节点系统进行功能仿真,并在Virtex-6 FPGA上完成了系统验证。结果表明,该设计实现了SpaceFibre总线节点的功能,串行传输速度可达3.125 Gbit/s,能够满足高速数据传输需求。     

武器装备研发成本补偿引入保险机制

随着我国军民融合武器装备研发生产体系的深度发展和社会主义市场经济体制的不断完善,武器装备研发中投入的研发成本面临很高的投资风险,成为困扰企业参与武器装备研发的重要因素。面对庞大的研发费用支出以及研发成本补偿措施不完善,企业要独自面对研发活动中的风险,这在一定程度上降低了企业参与装备研发的积极性。本文认为,通过保险机制的引入,鼓励企业为武器装备研发活动投保科技保险,同时,军方在对研发活动进行分析评判后,对企业的保费按比例进行分摊,能够在拓宽补偿途径的同时,利用保险分担企业研发过程中的风险,激发企业参与武器装备研发的热情,更好地为军队武器装备发展建设做出贡献。     

基于雾计算的路网-野区路径规划研究

针对路网、野区联合路径规划需求,提出了在雾计算平台上的路网-野区无缝衔接的路径规划方法,适用于路径规划区域同时覆盖城市道路与野区的情况.综合雾计算的特点,分析了路网-野区路径规划服务的应用方式.提出了适用于路网-野区环境下的启发函数,提供路径最短、时间最短两种模式的路径寻优算法.仿真和试验结果表明所提供的基于雾计算的路网-野区路径规划方法的可行性,能够满足路网-野区的路径规划需求.     

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.     

Adaptive subspace detection based on two-step dimension reduction in the underwater waveguide

In the underwater waveguide, the conventional adaptive subspace detector (ASD), derived by using the generalized likelihood ratio test (GLRT) theory, suffers from a significant degradation in detection per-formance when the samplings of training data are deficient. This paper proposes a dimension-reduced approach to alleviate this problem. The dimension reduction includes two steps: firstly, the full array is divided into several subarrays; secondly, the test data and the training data at each subarray are transformed into the modal domain from the hydrophone domain. Then the modal-domain test data and training data at each subarray are processed to formulate the subarray statistic by using the GLRT theory. The final test statistic of the dimension-reduced ASD (DR-ASD) is obtained by summing all the subarray statistics. After the dimension reduction, the unknown parameters can be estimated more accurately so the DR-ASD achieves a better detection performance than the ASD. In order to achieve the optimal detection performance, the processing gain of the DR-ASD is deduced to choose a proper number of subarrays. Simulation experiments verify the improved detection performance of the DR-ASD compared with the ASD.     

Formation and characterization of core-shell CL-20/TNT composite prepared by spray-drying technique

The core-shell 2,4,6,8,10,12-Hexanitro-2,4,6,8,10,12-hexaazaisowurtzitane/2,4,6-Trinitrotoluene (CL-20/TNT) composite was prepared by spray-drying method in which sensitive high energy explosive (CL-20) was coated with insensitive explosive (TNT). The structure and properties of different formulations of CL-20/TNT composite and CL-20/TNT mixture were characterized by scanning electron microscopy (SEM), Transmission electron microscopy (TEM), Laser particle size analyzer, X-ray photoelectron spectroscopy (XPS), X-ray diffraction (XRD), differential scanning calorimetry (DSC), impact sensitivity test and detonation performance. The results of SEM, TEM, XPS and XRD show that ϵ-CL-20 particles are coated by TNT. When the ratio of CL-20/TNT is 75/25, core-shell structure is well formed, and thickness of the shell is about 20–30 nm. And the analysis of heat and impact show that with the increase of TNT content, the TNT coating on the core-shell composite material can not only catalyze the thermal decomposition of core material (CL-20), but also greatly reduce the impact sensitivity. Compared with the CL-20/TNT mixture (75/25) at the same ratio, the characteristic drop height of core-shell CL-20/TNT composite (75/25) increased by 47.6% and the TNT coating can accelerate the nuclear decomposition in the CL-20/TNT composites. Therefore, the preparation of the core-shell composites can be regarded as a unique means, by which the composites are characterized by controllable decomposition rate, high energy and excellent mechanical sensitivity and could be applied to propellants and other fields.     

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.     

Evaluation of infrared camouflage effectiveness via a multi-fractal method

This paper reports an alternative approach to the evaluation of infrared camouflage effectiveness via a multi-fractal method. By calculating multi-fractal spectra of the target region and the background re-gions in an infrared image, the spectrum shape features and the discrete Fréchet distances among these spectra were used to analyze the camouflage effectiveness of the target qualitatively and quantitatively, and the correlation coefficients of the spectra were further used as the index of camouflage effectiveness. It was found that the camouflaged target had better camouflage effectiveness than the target without camouflage in the same one background, and the same one camouflaged target had different camouflage effectiveness in different backgrounds. On the whole, the target matching well with its background had high camouflage effectiveness value. This approach can expand the application of multi-fractal theory in infrared camouflage technology, which should be useful for the research of infrared camouflage mate-rials, the design of camouflage patterns as well as the deployment of military equipment in battlefield.