机动目标建模及机动检测算法

为解决机动目标跟踪问题,建立了非机动(匀速直线运动)和机动目标当前统计两种动态模型,并对机动目标当前统计模型的输入控制的估计进行了适当改进.同时对非机动模型的观测残差和机动模型的输入估计进行检验,以便准确检测目标机动.     

利用动态综合作战能力指数筹划海战兵力需求

针对目前海军作战兵力需求问题,建立了海军作战的物理模型,并提出了用动态综合作战能力指数筹划海战兵力需求的数学模型和算法,采用战例统计法和专家打分法计算出战斗力系数.并且以航空兵空中争夺为例进行了因素分析、参数选取、效能计算并得出了明确结论.计算结果表明,采用动态综合作战能力指数作为海战兵力需求指标是可行的;信息作战能力在现代海战中具有极其重要的作用.     

美军装备试验鉴定发展历程分析及启示

美军装备试验经历近百年的发展,已形成较为成熟的试验鉴定模式和管理评价体制,试验鉴定能力也处于世界领先水平.美军在装备发展历程中的经验做法十分值得学习和借鉴.本文分析了美军装备试验鉴定发展历程和特点,研究了其试验组织结构的科学构成和运行机制,归纳总结了美军装备试验发展的客观规律和科学经验.在此基础上,得到了顺应装备发展趋...     

基于测试码并行的同步时序电路故障模拟方法

将组合电路故障模拟的一些加速技术推广到时序电路故障模拟中,提出并实现了一个功能块级的基于测试码并行的同步时序电路故障模拟方法,对部分ISCAS89 Benchmark电路的模拟结果表明,该故障模拟方法有较好的性能.     

箭（弹）级间螺栓法兰连接结构准静载失效实验与数值仿真研究

基于火箭(导弹)级间螺栓法兰连接结构,简化设计并制作了一组原理性实验件,设计准静载加载实验测试系统,进行了两次准静载失效实验,并利用ABAQUS软件建立对应的有限元模型。实验中设计了螺栓力响应信号采集传感器,获得了螺栓力响应数据、加载力与加载位移等多组关键数据。根据实验效果和实测数据,分析了连接结构在准静载荷载作用下的失效机理,并对比验证了有限元模型数值模拟效果和精度与实验吻合较好。研究结论可为箭(弹)级间连接结构承载能力和失效实验设计提供参考。     

Holonic-C2组织决策分配及演化方法

为了有效发挥指挥控制(Command and Control, C2)组织集中式决策和协作式决策的决策优势,对具有决策权限动态变化能力的Holonic-C2组织的决策分配问题进行研究。针对群决策中专家固定权重的主观性太强的缺点,提出基于专家权威性和意见一致性相结合的专家组选择方法,提高了决策分配过程中多属性决策的客观合理性;针对决策分配的动态演化问题,提出基于多阶段决策的决策模式演化机制,在考虑属性前后阶段的变化的基础上,给出相邻阶段决策模式跃迁方法。仿真结果表明,所提方法能够给出相对客观的决策模式的优劣排序以及多阶段的演化路线,从而证明了方法的可行性和有效性。     

Study on performance degradation and failure analysis of machine gun barrel

An increase in the use of the gun barrel will cause wear of the inner wall, which reduces the muzzle velocity and the spin rate of the projectile. The off-bore flight attitude and trajectory of the projectile also change, affecting the shooting power and the accuracy. Exterior ballistic data of a high-speed spinning projectile are required to study the performance change. Therefore, based on the barrel's accelerated life test, the whole process of projectile shooting is reproduced using numerical simulation technology, and key information on the ballistic performance change at each shooting stage are acquired. Studies have shown that in the later stages of barrel shooting, the accuracy of shooting has not decreased significantly. However, it is found that the angle of attack of the projectile increases as the wear of the barrel increases. The maximum angle of attack reaches 0.106 rad when the number of shots reaches 4300. Meanwhile, elliptical bullet hole has appeared on the target at this shooting stage. Through combining external ballistic theory with simulation results, the primary reason of this phenomenon is found to be a significant decrease in the muzzle spin rate of the projectile. At the end of the barrel life, the projectile muzzle spin rate is 57.5% lower than that of a barrel without wear.     

Priori information analysis of optocoupler accelerated degradation experiment based on failure mechanism verification test

The optocoupler is a weak link in the inertial navigation platform of a kind of guided munitions. It is necessary to use accelerated storage test to verify the storage life of long storage products. Especially for small sample products, it is very important to obtain prior information for the design and implementation of accelerated degradation test. In this paper, the optocoupler failure mechanism verification test is designed and the experimental results are analyzed and the prior information is obtained. The results show that optocouplers have two failure modes, one is sudden failure and the other is degradation failure; the maximum temperature stress of optocoupler can't exceed 140 °C; the increase of leakage current of optocoupler is caused by movable ions contaminating the LED chip. The surface leakage current is proportional to the adsorption amount. The increase of leakage current makes p-n junction tunneling effect occur which LEDs the failure of the optocoupler. The lifetime distribution model of the optocoupler is determined by the failure physics. The lifetime of the optocoupler is subject to the lognormal distribution. The degeneracy orbit of the optocoupler leakage current is described by a power law model. The estimated values of the orbital parameters are initially calculated and the parameters of its life distribution function are deduced. The above information lays a good foundation for the optimization design and data processing of the accelerated degradation experiment.     

美国陆军作战试验部队管理体系研究

作战试验部队是试验鉴定力量体系的重要支撑,是完成装备作战试验的直接载体。美国在装备试验与鉴定方面走在世界前列,建立了一整套行之有效的管理体制,陆军实行试验与鉴定的一体化管理,具有独立的作战试验鉴定部门,没有编设专业化的作战试验部队,试验任务主要根据装备的特性选取未来典型用户的作战部队在真实对抗环境中完成。作战试验部队主要参加作战评估、初始作战试验与评价以及后续作战试验与评价三个阶段的作战试验,在一体化试验小组的协调下,依托靶场完成试验训练任务。本文主要通过对美国陆军试验部队的研究,分析了美国陆军作战试验与鉴定发展概况,重点研究了作战试验部队管理体系,并从整个试验与鉴定系统归纳总结作战试验部队管理及相关工作的主要做法。     

美国应对外空国际条约的做法简析

针对现行国际空间法存在的诸多漏洞和缺陷,国际空间大国积极利用这些漏洞寻求开展外空试验的依据,并规避法律的约束以发展外空武器装备,使得外空存在被武器化的风险,外空军备竞赛日益激烈。因此,研究并利用外空条约、关注空间大国开展外空试验的现实做法,可以为开展外空活动提供借鉴和依据。本文重点研究了美国海基反卫试验和轨道快车试验,从试验背景、目的、对外口径以及对外反应几个方面,综合对比分析了试验的现实做法,剖析了美国应对外空条约的做法,从技术上、政策上和法律上得出了如何应对的方法和途径。研究成果可为我国合理合法地开展外空行动提供借鉴,从而赢得国际社会的认可。