武器装备全寿命费用宏观控制的系统动力学模型

以武器装备作战能力差距为牵引,以全寿命周期阶段对作战能力的影响为主要依据,建立了基于系统动力学的武器装备全寿命费用控制分析模型,客观、合理地描述了全寿命周期各阶段之间的相互影响,并对武器装备全寿命费用宏观费用控制问题进行了仿真实验分析。     

REBO模型的平衡态分子动力学模拟

为了得到合适的"计算机实验"的"试样"进行固体炸药冲击起爆现象的分子动力学研究,对REBO模型进行了NVE,NVT两种平衡态分子动力学模拟;作为对比,同时还进行了不施加任何人工干预,系统的演化完全由运动方程驱动的分子动力学模拟,讨论了根据对"试样"的不同要求选择适当模拟方法的原则。     

网络中心战的系统动力学模型研究

网络中心战是信息时代的一种新的作战模式,深入研究其特点及对作战的影响具有十分重要的意义。明确了网络中心战的基本概念,基于系统动力学理论,针对网络中心战对空军作战的影响,建立了相应的系统动力学模型,通过不同仿真结果的比较,阐明了网络中心战的主要特点,并做出了相应的对策分析。     

基于SD的两栖坦克连水上火力支援行动分析

围绕两栖坦克连水上火力支援行动的作战特点,着眼于充分发挥两栖坦克火力和机动的优势,在"非接触作战、非线性作战"理论的指导下,运用系统动力学方法和兰切斯特战斗理论,建立两栖坦克连水上火力支援行动的系统动力学模型,探索装甲兵在应急作战中运用的新模式和作战的新方法,为指挥员科学使用这一战术手段提供有效地辅助决策支持。     

大攻角下基于卡尔曼滤波的大气参数修正算法

针对新一代航空飞行器在大攻角飞行时大气数据系统测量精度严重下降问题,提出了基于卡尔曼滤波的大气参数修正算法。该算法利用大气数据测量信息和惯性导航信息,基于飞行器力学方程构建卡尔曼滤波器,通过卡尔曼滤波的方法实现对大气参数的修正。仿真结果表明,经卡尔曼滤波修正后的大气参数能够有效消除大攻角下原始大气参数的剧烈波动性误差,并与真实大气参数吻合较好,有效的提高了大气数据系统在大攻角飞行状态下的测量精度和可靠性。     

Research and development of training pistols for laser shooting simulation system

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.     

Theoretical calculation and experimental study on the interaction mechanism between TKX-50 and AP

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.     

Late Medieval Lance Use: Mounted Combat and Martial Arts in Western Europe from the 14th to the 16th Century

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.     

反电动势对无扰载荷航天器精确定向的影响

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。     

基于改进粒子群算法的自动机性能评估

由于自行高炮自动机状态监测中缺乏行之有效的机构性能评估手段,引入了改进粒子群算法。建立了自动机动力学模型,对后坐过程进行了动力学仿真,确定了反映机构性能的浮动曲线特征量。针对粒子群算法收敛速度慢、精度低等缺陷,对其进行改进,并结合曲线特征量对自动机性能参数进行了评估。结果表明:改进后粒子群算法的算法收敛性和结果精度都有明显的改善,有效实现了自动机的性能参数评估。