基于行小波编码的纹理隐藏三维地形数据算法

讨论利用纹理图像隐藏高程信息来保护三维地形数据的信息隐藏技术。首先提出了改进的基于行小波变换及其编码,在保持地形形状和起伏特征的前提下实现高程数据的极低比特率低存储压缩。通过研究可嵌入隐藏信息的小波系数集合生成方法并结合基于视觉系统(HVS)小波域量化噪声的视觉权重(JND)分析技术,提出了自适应确定信息嵌入强度的方法。由于隐藏过程采用分组密码Rijndael生成单向Hash函数,信息隐藏算法高度安全、可以公开。     

【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。     

基于改进二进制蝙蝠算法的装备资源保障规划

针对联合作战环境下的装备资源精确保障协同规划问题,考虑以所有保障任务完成时间最短为目标,以保障任务的执行时序和资源需求、保障编组占用冲突,以及资源平台能力更新机制等复杂条件为约束,构建数学模型,提出了基于动态列表调度(Dynamic List Scheduling,DLS)和自适应进化变异二进制蝙蝠算法(Adaptive Mutation Binary Bat Algorithm,AMBBA)的混合装备资源协同保障规划方法.通过动态列表调度选择当前执行保障的任务,在二进制蝙蝠算法寻优中引入自适应学习因子以平衡全局搜索和局部搜索能力,通过在当前可用资源集中搜索最优解为选定任务分配资源,以复杂地域联合作战为例仿真并验证规划效果,结果显示,所提方法可对大规模装备资源协同分配保障问题进行精确高效求解.     

基于效能优先原则的武器决策方法研究

武器站是适应未来战场快速反应和应急机动等多功能要求的新型武器系统,其火力配置多种武器组合,当发现攻击目标时,选择哪种武器进行打击,目前主要通过作战人员依靠人工经验进行决策.针对上述问题,提出了基于效能优先原则的武器决策方法,该方法充分考虑作战任务、目标属性、天气条件、打击费用等影响因素,构建了武器决策效费比模型,通过作战实例分析,验证了该模型可有效解决武器站在多个作战条件下的武器决策问题.     

美军国防采办政策改革及启示

美军在长期的国防采办实践中,经过不断改革和多次调整,逐步形成了较为完备的国防采办政策制度及管理体系,其有益经验和做法具有开创性和引领作用。尤其是自2018年启动重组国防采办组织管理体制以来,美军在国防战略调整的牵引下,先后发布多份新版采办文件,从政策体系、采办程序、业务领域等方面作出了重大改革调整,初步形成了“1+6+14”的政策体系架构。本文主要对美军国防采办政策的改革举措、背景及动因进行深入分析,总结美军国防采办政策改革的特点规律,试图通过研究美军国防采办改革的动向,探寻信息化条件下国防采办的特点及规律,并结合军队信息化装备采购实际提出思考与建议,以期为深化军队改革提供一定借鉴。     

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.     

Design and analysis of a scheme for the naval gun test shell entering the bore

The test shell without projectile belt is widely used in the teaching, inspection and maintenance of modern automatic naval guns. In order to ensure the normal work of each mechanism, it is very important to design the buffer and limit of the test shell during the process of entering the bore. Taking a certain type of medium caliber naval gun as the research object, the design of colloidal fluid damper and cartridge lock was proposed to ensure the reliability of entering the bore and closing the breechblock. By combining the simulation methods of computational fluid dynamics (CFD) and multibody system dy-namic (MBD), it was analyzed whether the structural design can meet the engineering requirements. The research results show that the colloidal fluid damper can dissipate a large amount of kinetic energy of the shell, and the cartridge lock can limit the rebound movement. The combination of the two ensures the smooth process of closing the breechblock. The research provides a design method for the process of the test shell entering the bore, and provides theoretical support for the feasibility of the method.     

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.     

Quasi-steady aerodynamic characteristics of Terminal Sensitive Bullets with short cylindrical portion

The aerodynamic characteristics are vital for short cylindrical Terminal Sensitive Bullets(TSB)with low aspect ratio,especially in terminal trajectory.Currently,there is little research in terms of the TSB and short cylinder with two free ends,and particularly in this trajectory,where the scanning angle β and roll angle α vary over a broad range between 0° and 180°.In this work,wind tunnel experiments are first conducted to learn the effects of Reynolds number and scanning angle on aerodynamic parameters for short cylinder with aspect ratio L/D = 1.Similar to infinite cylinder,for the short cylinder with two free ends,the drag crisis phenomenon still exists in the critical regime 1.7 × 105 ≤ Re ≤ 6.8 × 105.Then 3D simulations are performed to demonstrate the aerodynamic characteristics of short cylinder and TSB over a broad range of Re,L/D,α and β.The sensitivity analysis of time step and grid are presented as well.When β=0°,for short cylinder,the drag crisis phenomenon was also observed in the simulation,but not as obvious as in the wind tunnel test.In some attitudes,there is an obvious Kármán vortex in the wake of short cylinder and TSB.The correlation between time-averaged aerodynamic coefficients and L/D,Re,α&β is discussed.The vortex shedding frequency and shear layer behavior are obtained for quasi-steady and unsteady flow.Finally,the effect of end's shape on drag reduction and vortex shedding frequency is analyzed.