车辆座椅变刚度变阻尼减振的研究

基于双磁流变阻尼器构建了变刚度变阻尼的座椅半主动减振系统,建立了人体-座椅的2自由度动力学模型;对该半主动变刚度变阻尼系统的座椅减振方式采取了开关控制算法.将系统模型在MATLAB—SIMULINK中进行相应的建模仿真,并与被动减振模型进行对比分析.仿真结果表明,人体加速度均方根值要减小72.8%,人体垂直位移均方根值要减小18.4%,大幅度降低了人体所受的振动强度,能有效地改善座椅的减振效果.     

火控系统中惯性技术的应用

对武器中火控系统应用惯性技术的原因、特点进行了简要的介绍,并对火控系统中的基准设备的配置方案进行了简单的介绍。     

带初始前置角和末端攻击角约束的偏置比例导引律设计以及剩余飞行时间估计

针对导弹飞行过程中受到外部干扰导致前置角变化较大的问题,设计了满足任意初始前置角和末端攻击角度约束的偏置比例导引律,并对该导引律下系统参数的收敛性给出了证明。基于现有分段迭代求解剩余飞行时间的方法进行拓展,解决了现有分段迭代求解方法在前置角等于π/2 rad时存在奇点的问题,并用该改进方法给出了该导引律的剩余飞行时间估计。对提出的导引律和改进的分段迭代求解方法进行仿真,结果表明：该导引律能够满足任意初始前置角和末端攻击角度约束下导弹的脱靶量和末端角度要求,且在飞行末端加速度指令收敛至0;与以往研究结果相比,该导引律在前置角大于π/2 rad时能够实现对导弹的更有效控制;使用改进的分段迭代求解方法对提出的导引律进行剩余飞行时间估计,估计误差小,误差收敛快。仿真结果验证了该偏置比例导引律和剩余飞行时间估算方法的有效性。     

多高超声速导弹协同末制导律及可行初始位置域研究

针对多高超声速导弹以指定落角对目标进行饱和攻击的问题,提出一种具有攻击角度和攻击时间约束的末制导律,并基于此对导弹的末制导可行初始位置域进行研究。建立三维空间导弹运动模型,分别通过纵向通道和侧向通道制导指令实现落角和攻击时间控制,构成三维协同末制导律。考虑导弹过载和末速约束,采用上述制导律,以导弹末制导初始位置的坐标为设计变量,以实际攻击时间与理想攻击时间差为性能指标函数,建立并求解优化模型,得到导弹一维及二维可行末制导初始位置域。仿真结果表明:该三维协同制导律可使多导弹在同一指定时间以指定落角命中目标; 该位置域求解方法可求得给定约束条件下的各导弹末制导可行位置域。     

The Effect of Nanotube Content and Orientation on the Mechanical Properties of Polymer–Nanotube Composite Fibers: Separating Intrinsic Reinforcement from Orientational Effects

We have measured the mechanical properties of coagulation‐spun polymer–nanotube composite fibers. Both the fiber modulus, Y, and strength, σ_B, scale linearly with volume fraction, V_f, up to V_f ～10%, after which these properties remain constant. We measured dY/dV_f = 254 GPa and dσ_B/dV_f = 2.8 GPa in the linear region. By drawing fibers with V_f < 10% to a draw ratio of ～60%, we can increase these values to dY/dV_f = 600 GPa and dσ_B/dV_f = 7 GPa. Raman measurements show the Herman's orientation parameter, S, to increase with drawing, indicating that significant nanotube alignment occurs. Raman spectroscopy also shows that the nanotube effective modulus, Y_Eff, also increases with drawing. We have calculated an empirical relationship between the nanotube orientation efficiency factor, η_o, and S. This allows us to fit the data for Y_Eff versus η_o, showing that the fiber modulus scales linearly with η_o, as predicted theoretically by Krenchel. From the fit, we estimate the nanotube modulus to be; Y_NT = 480 GPa. Finally, we show that the fiber strength also scales linearly with η_o, giving an effective interfacial stress transfer of τ = 40 MPa and a nanotube critical length of l_c=1250 nm. This work demonstrates the validity of the Cox‐Krenchel rule of mixtures and shows that continuum theory still applies at the near‐molecular level.     

初始啁啾对光纤中传播的飞秒光孤子的影响

采用分步傅里叶变换作为数值模拟的方法,以二阶飞秒光孤子和基态飞秒光孤子为例,讨论了初始啁啾对光纤中传播的飞秒光孤子的时域特征和频谱结构的影响,概括出如下的结论:初始啁啾通过影响飞秒光孤子谱线的红移,而对飞秒光孤子由拉曼效应引发的脉冲延迟产生较大影响,正的初始啁啾使脉冲延迟加剧,负的初始啁啾使脉冲延迟减小.     

An investigation on TCP large initial window

Transport layer implicates a position where satellite networks form one integrated component of hybrid Internet architecture in today's advance technology. However, the Internet has emerged with an important new class of applications that exhibits significant variations of transmission rate over time. Variable‐rate traffic poses a new challenge for transmission control protocol that provides congestion control, especially for applications that need to share the limited capacity of a bottleneck over a long delay Internet path (e.g. paths that include satellite links). Variable‐rate traffic can be produced by persistent transmission control protocol connections and can be impacted by the initial window at the start or during the restart of a session. Current transport research issues are identified related to larger initial window to highlight the expected performance benefits and derive the implications on the design of geostationary satellite Internet systems as the network evolves toward a next‐generation Internet. Copyright © 2013 John Wiley & Sons, Ltd.     

便携式地空导弹海上作战使用研究

分析舰船运动特性对便携式地空导弹射击的影响,建立求解导弹初始弹道运动学参量的数学模型.针对某型便携式地空导弹进行舰船平台弹道特性分析,结果表明便携式地空导弹可以在舰船平台上实施射击.     

齿轮裂纹对啮合刚度的影响分析

通过对三维轮齿接触有限元分析,建立了正常和齿根与分度圆处不同裂纹故障的直齿圆柱齿轮三维实体有限元模型;通过对其啮合接触分析,求得不同状态下齿轮整个啮合过程的轮齿啮合综合刚度.分析结果表明:齿根裂纹对啮合刚度的影响要大于分度圆裂纹的影响.这对分析裂纹故障对齿轮啮合刚度的影响具有一定的指导作用.     

电容器参数对最佳发射初始位置影响的研究

目前国内外电磁发射技术发展迅速,论述了电磁炮在军事上的应用,详细介绍线圈炮的工作原理与分类,并通过试验研究发射初始位置对炮口初速和相应效率的影响.