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751.
《防务技术》2020,16(3):530-534
Firearm shooting simulators are effective means for training the personnel in armed forces, police and shooting athletes. Shooter–weapon is a complex biomechanical system, therefore the best training quality is achieved when the process of a weapon shot is reconstructed in a training simulator and its training weapon mimics the (feeling) perception of the real weapon usage. Dynamics of motions of a handgun simulator held in the hand of a shooter by its grip during the shot is analysed theoretically and experimentally. Breech lock mechanism of the simulator is actuated pneumatically by supplying compressed air in pulses from external pressure source. Analysis of the obtained simulation results and experimentally recorded motion parameters of the training weapon body reveals that application of pneumatic drives is a reasonable option to simulate recoil perception of a pistol.  相似文献   
752.
《防务技术》2020,16(5):1062-1072
Recent years have seen an explosion in graph data from a variety of scientific, social and technological fields. From these fields, emotion recognition is an interesting research area because it finds many applications in real life such as in effective social robotics to increase the interactivity of the robot with human, driver safety during driving, pain monitoring during surgery etc. A novel facial emotion recognition based on graph mining has been proposed in this paper to make a paradigm shift in the way of representing the face region, where the face region is represented as a graph of nodes and edges and the gSpan frequent sub-graphs mining algorithm is used to find the frequent sub-structures in the graph database of each emotion. To reduce the number of generated sub-graphs, overlap ratio metric is utilized for this purpose. After encoding the final selected sub-graphs, binary classification is then applied to classify the emotion of the queried input facial image using six levels of classification. Binary cat swarm intelligence is applied within each level of classification to select proper sub-graphs that give the highest accuracy in that level. Different experiments have been conducted using Surrey Audio-Visual Expressed Emotion (SAVEE) database and the final system accuracy was 90.00%. The results show significant accuracy improvements (about 2%) by the proposed system in comparison to current published works in SAVEE database.  相似文献   
753.
《防务技术》2020,16(4):825-833
The combination of 5,5′-bistetrazole-1,1′-diolate (TKX-50) and ammonium perchlorate (AP) can make greater use of the chemical energy of TKX-50 based energetic materials. The research on the interaction mechanism between TKX-50 and AP is very important for designing TKX-50-AP compounds and judging the formation feasibility of composite particles, which can lay a theoretical foundation for the preparation of TKX-50-AP mixed crystals and the application of TKX-50 in propellant, propellant and explosive. Herein, in order to research the interaction mechanism between TKX-50 and AP, density-functional theory calculation was applied to optimize three configurations of TKX-50-AP compounds. The geometry structure, electrostatic potential and binding energy of the compounds were predicted, and the electronic density topological analysis was also carried out. Then TKX-50-AP mixed crystals structures were constructed, and the radial distribution function of H–O and H–N in mixed crystals was calculated. Finally, solvent/non-solvent method was applied to prepare TKX-50-AP composites, and the infrared spectroscopy and the non-isothermal decomposition performance of the composites were characterized. Results show that the superposition of positive charges in TKX-50 molecule and negative charges in AP makes the electrostatic potential distributions of TKX-50-AP compounds different from that of TKX-50 and AP. The interaction energies of TKX-50-AP 1, TKX-50-AP 2 and TKX-50-AP 3 are 39.743 kJ/mol, 61.206 kJ/mol and 27.702 kJ/mol, respectively. The interaction between TKX-50 molecules and AP molecules in TKX-50-AP mixed crystals both depends on hydrogen bonds and van der Waals force, and the number and strength of hydrogen bonds are significantly greater than that of van der Waals force. The composition of AP and TKX-50 makes the absorption peak of the five-membered rings and NH3OH+ of TKX-50 shift to low wavenumber in the infrared spectroscopy. In general, TKX-50 interacts with AP via hydrogen bonds and van der Waals force, and the calculated results are in good agreement with the experimental results. The composition of TKX-50 and AP can also prolong the decomposition process.  相似文献   
754.
将在某一频率下或某一频段内对封闭声腔声势能起主要作用的一阶或几阶声辐射模态定义为耦合封闭声腔的主导声辐射模态。准确认定主导声辐射模态至关重要,直接影响有源控制效果。然而,现有的主导声辐射模态确定方法,要么仅考虑辐射效率的作用而忽视模态幅度的影响,要么就需要用到结构模态信息,难以实现工程应用。基于此,综合运用计算和测试手段,全面考虑辐射效率和模态幅度两个因素,提出了一种基于“初选—预留—后验”的主导声辐射模态确定方法,并通过实验研究证明了该方法的有效性和可行性。结果表明:提出的确定方法能够准确认定主导声辐射模态,确定过程中不需要用到辐射体的结构模态信息,可用于指导控制目标选取或重构封闭声腔声势能。  相似文献   
755.
为了提高海洋声学快速场模型在近场区域的计算精度,分析了影响经典快速场模型精度的因素,主要包括Bessel函数近似、忽略内行波项以及在水平距离最远处波数采样率过低,这些因素导致快速场模型近场误差较大、远场水平距离最远处结果不正确(计算结束后需要去除水平距离后段的声场)。提出能够提高经典快速场模型近场计算精度的改进模型,改进部分主要是采用保留内行波项的近似Bessel函数,再将近场上下两个基于声源点与对称轴的三角形区域用波数积分解(使用精确Bessel函数)覆盖。算例测试结果表明:与经典快速场模型相比,改进模型可在绝对时间增加较少的情况下,显著提高近场计算精度,综合性能更优;与波数积分法相比,改进模型在误差为同量级的情况下,积分时间大幅降低,实际应用价值更高。  相似文献   
756.
针对无人机在单站测角测距的目标定位过程中受无人机姿态角误差影响较大的问题,提出一种对辅助信标进行探测并与惯性传感器相结合的无人机姿态求解方法。建立基于容积卡尔曼滤波的惯性传感器姿态求解模型,采用梯度下降法对基于辅助信标的无人机位姿参数进行求解,并综合它们的结果对无人机的姿态偏差进行估计和校正,最后完成了不同视场条件下的目标定位和仿真计算。结果表明,所提方法对无人机目标定位精度有明显提高。  相似文献   
757.
Despite the lance’s status and the amount of attention the couched lance has received in historiography, study of its martial art has been neglected. The various lance types and techniques used by western European cavalry have only recently begun to receive scholarly attention. Additionally, Medieval European lance use has too often been studied in isolation, without an adequate understanding of the idiosyncratic and asymmetrical dynamics of mounted combat. Although the charge with the couched lance was a valid tactic, it was only one of many. Light and heavy lances were used in one hand or two to trip, block, unhorse, and wrestle. These techniques were governed by the harsh laws of distance, speed, impact, iron, and asymmetry. By utilizing the surviving Fechtbücher and several Peninsular and Near Eastern sources, a brief foray into the diverse techniques of lance use and their purposes has been attempted here.  相似文献   
758.
In the context of restricted budgetary resources and the growing cost of maintenance, repair, and overhaul (MRO) activities, a major issue for modern armed forces is to sustain defense platforms. A possible method consists of realizing economies of scale through the concentration of maintenance activities, which involves the spatial reorganization of existing industrial sites dedicated to MRO. This article provides a formalized framework to discuss the optimal organization for the MRO of defense platforms in space. The public planner organizes the maintenance of defense platforms with only two possible spatial configurations. In the dispersed configuration, two industrial production units in charge of the maintenance optimally cover space, whereas in the concentrated configuration, a unique industrial unit covers space. Focusing on the tipping point between the two configurations, the balance of forces between agglomeration and dispersion in defense support activities is described and discussed. On the one hand, economies of scale provide an opportunity to optimize defense support costs, favoring concentration in a unique industrial unit. On the other hand, space causes dispersion to reduce both transport costs and operational social costs. This trade-off illustrates a general principle in spatial economics with an application to MRO production in the French case.  相似文献   
759.
发展显微成像方法获得空间分辨率为1.57 μm/pixel的近场射流瞬态图像,分析超声速气流中液体横向射流表面波演化规律。采用流体体积法获得射流的三维形态及近场流场特征,研究近场流场结构及气液作用。射流的一次破碎过程主要有表面破碎和液柱破碎。其中表面破碎由气液剪切引起的K-H不稳定主导,液柱破碎由气液加速引起的R-T不稳定主导;射流柱表面局部压力的脉动是诱导产生射流迎风面表面波并促使其沿射流方向发展的主要原因;射流柱与超声速气流作用形成背风面回流,近壁面液雾主要由表面破碎及背风面回流输运的液滴组成。  相似文献   
760.
无扰载荷航天器中非接触式作动器反电动势会引起有效载荷模块与支持模块之间的耦合,影响有效载荷模块的精确定向性能。通过建立无扰载荷航天器的耦合动力学模型,分析非接触式作动器反电动势对有效载荷模块精确定向性能的影响。考虑六支杆立方构型无扰载荷接口,结合拉格朗日方程和牛顿欧拉方法建立有效载荷模块平台动力学模型。推导非接触式作动器的输出力模型,并引入有效载荷模块平台动力学模型,给出考虑非接触式作动器反电动势的耦合动力学模型。将支持模块上飞轮动静不平衡引起的谐振作为干扰力矩,建立了无扰载荷航天器在轨定向状态的Simulink仿真模型。仿真结果表明,反电动势系数越大,干扰力矩对有效载荷模块的影响越大,有效载荷模块精确定向精度越低。  相似文献   
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