地基刚度变化对车辆动力特性的影响

根据两自由度车辆振动模型和道路多层离散体系模型,建立了车辆-道路垂向耦合动力分析模型,推导出了车辆-道路系统的动力平衡方程组,并对动力平衡方程组进行了编程求解,分析了地基刚度变化对车辆动荷载和车身加速度的影响.分析表明:地基刚度变化对车身加速度影响不大,在地基刚度达到某一临界值后一定的范围内,地基刚度的变化对动荷系数影响也不再显著,否则,要对地基进行处理.     

三维多目标纯测向无源定位方法

针对多传感器测向定位中方位配对的困难,提出分两步的三维多目标纯测向定位方法.该方法先利用方位信息,粗略估计目标二维位置,并采用方位角误差进行粗略的目标真伪判别,再采用蛙跳式梯度法精确求解目标的三维位置,并利用方位角与俯仰角偏差对目标真伪进行判别.仿真结果表明,该方法能快速地以较高概率、较高精度对多目标进行定位.     

采用空气轴承的大行程快速刀具伺服系统

随着对结构化超精密部件需要的不断增加,出现了加工具有高的表面光洁度以及形状精度的非旋转对称镜片的新技术。根据现有的快速刀具伺服系统,研制出了最大行程为16mm的新型快速刀具伺服系统(图1)。以前的快速刀具伺服系统采用了弹性导向机构,而现在的快速刀具伺服系统则采用了空气轴承,并且用了一个高频直线电机来驱动这个系统。由于采用了一个新的功率放大器,使得这个系统能够最高达到100Hz的频率以及1mm的振动幅度。这篇文章给出了这种新型快速刀具伺服系统的技术细节。     

调炮精度检测中双经纬仪优化布站方法

针对“双经纬仪法”检测调炮精度中随机布站使测量系统达不到最佳测量精度的问题,提出了一种优化布站方法.根据火炮调炮范围确定了调炮精度检测中的测量区域,推导出了双经纬仪测量系统对于该测量区域的平均测量不确定度公式.结合某型火炮设计了基于遗传算法的具体优化过程,对测量系统的3个位置参数进行优化,得到最佳测量布局,并通过仿真试...     

基于区间数理论的空战目标威胁评估

针对空战目标威胁评估问题,提出了一种新的基于区间数理论的评估方法。在分析了现有的目标威胁评估方法中距离威胁模型存在不足的基础上,提出了改进的距离威胁模型。给出了区间数特征向量法求解威胁指标权重的计算步骤,建立了基于区间数理论的空战目标威胁评估的数学模型。最后给出了仿真算例,仿真结果表明该方法是合理和有效的。     

Churchill's naval holiday: Arms control and the Anglo‐German naval race, 1912–1914

Brian Johnson, The Secret War. London: BBC, 1978. Pp. 352; £6.50.

R. V. Jones, Most Secret War: British Scientific Intelligence 1939–45. London: Hamish Hamilton, 1978. Pp. xx + 556; £7.95.

Solly Zuckerman, From Apes to Warlords 1904–46. London: Hamish Hamilton, 1978. Pp. 00 (Information not available from publisher); £8.50.

Adrian Preston, ed., General Staffs and Diplomacy before the Second War. London: Croom Helm, 1978. Pp. 138; £5.95.

W. G. F. Jackson. ’Overlord’: Normandy 1944. London: Davis Poynter, 1978. Pp. 250; £6.75.

Richard K. Betts, Soldiers, Statesmen, and Cold War Crises. Cambridge, Mass. and London: Harvard University Press, 1977. Pp. 292 + index + appendices; Np.

Gerard J. Mangone, Marine policy for America—The United States at Sea. Lexington, Mass.: Lexington Books, 1977. Pp. 370, £17.50.

F. M. Richardson, Fighting Spirit. London: Leo Cooper, 1978. Pp. 189 + xv; £7.50.

Allen R. Millet, Ed., A Short History of the Vietnam War. London &; Bloomington: Indiana University Press, 1978. Pp. 169; £2.75.

Robert P. Berman, Soviet Airpower in Transition. Washington: Brookings, 1978. Pp. 82; $2.95 (Paper).     

Comparison between constant‐stress and step‐stress accelerated life tests under Time Constraint

By running life tests at higher stress levels than normal operating conditions, accelerated life testing (ALT) quickly yields information on the lifetime distribution of a test unit. The lifetime at the design stress is then estimated through extrapolation using a regression model. In constant‐stress testing, a unit is tested at a fixed stress level until failure or the termination time point of test, whereas step‐stress testing allows the experimenter to gradually increase the stress levels at some prefixed time points during the test. In this work, the optimal k‐level constant‐stress and step‐stress ALTs are compared for the exponential failure data under complete sampling and Type‐I censoring. The objective is to quantify the advantage of using the step‐stress testing relative to the constant‐stress one. Assuming a log‐linear life–stress relationship with the cumulative exposure model for the effect of changing stress in step‐stress testing, the optimal design points are determined under C/D/A‐optimality criteria. The efficiency of step‐stress testing to constant‐stress one is then discussed in terms of the ratio of optimal objective functions based on the information matrix. © 2013 Wiley Periodicals, Inc. Naval Research Logistics 00: 000–000, 2013     

基于双FPGA+DSP全姿态指示仪系统设计

针对全姿态指示仪对画面显示和信号处理的要求,系统采用双FPGA+DSP的硬件体系结构,把整个任务分成信号采集与预处理模块、图形与字符轮廓生成模块和显示模块.介绍了系统的原理框图、FPGA2的实现结构以及改进的边标志填充算法.本系统解决方案满足了画面逼真显示和信号实时处理的要求,并且具有很好的可靠性和重构性.