Technical note: An improved range chart for normal and long‐tailed symmetrical distributions

The distribution of the range of a sample, even in the case of a normal distribution, is not symmetric. Shewhart's control chart for range and other approximations for range from skewed distributions and long‐tailed (leptokurtic) symmetrical distributions assume the distribution of range as symmetric and provide 3 sigma control limits. We provide accurate approximations for the R‐chart control limits for the leptokurtic symmetrical distributions, using a range quantile approximation (RQA) method and illustrate the use of the RQA method with a numerical example. As special cases, we provide constants for the R‐chart for the normal, logistic, and Laplace distributions. © 2007 Wiley Periodicals, Inc. Naval Research Logistics, 2008     

潜艇攻击鱼雷最小射程圆内目标的方法

针对潜艇攻击鱼雷最小射程圆内目标的方法问题,首先,给出了不同自导方式下鱼雷最小射程的计算方法,并分析其对鱼雷攻击的影响;然后,依据鱼雷二次转角射击弹道过程,建立了鱼雷二次转角射击通式,并分析了鱼雷二次转角射击需满足的约束条件;在此基础上,深入研究了潜艇攻击鱼雷最小射程圆内目标的具体方法。最后通过实例验证了攻击方法的可行性和有效性。     

某尾翼式火箭增程迫弹飞行失稳原因分析

针对某尾翼式火箭增程迫弹弹道飞行失稳的现象,建立了火箭增程迫弹的六自由度弹道模型,仿真分析了该弹丸的摆动角变化规律、全弹道静稳定度、动态稳定度,共振转速、平衡转速等,最终确定共振为该弹飞行失稳的主要原因。为避免弹丸共振的产生,研究确定了该弹的最佳转速范围,通过最大射程及密集度试验结果表明平衡转速为8r～10r时,发动机作用对弹丸飞行影响较小,密集度最好。     

Estimating component characteristics from system failure‐time data

Suppose that failure times are available from a random sample of N systems of a given, fixed design with components which have i.i.d. lifetimes distributed according to a common distribution F. The inverse problem of estimating F from data on observed system lifetimes is considered. Using the known relationship between the system and component lifetime distributions via signature and domination theory, the nonparametric maximum likelihood estimator _N(t) of the component survival function (t) is identified and shown to be accessible numerically in any application of interest. The asymptotic distribution of _N(t) is also identified, facilitating the construction of approximate confidence intervals for (t) for N sufficiently large. Simulation results for samples of size N = 50 and N = 100 for a collection of five parametric lifetime models demonstrate the utility of the recommended estimator. Possible extensions beyond the i.i.d. framework are discussed in the concluding section. © 2010 Wiley Periodicals, Inc. Naval Research Logistics, 2010     

大动态范围星载导航接收机AGC电路性能分析与优化设计

"导航战"条件下要求接收机具有较强的抗干扰性能,射频电路是制约接收机抗干扰性能的瓶颈之一。针对星载导航接收机的特点,同时兼顾弱信号接收与强信号接收的情况,以接收机在整个信号范围内工作时能够抑制的干信比J最大为优化目标,分析了电路允许实现的最大干信比Jmax及射频电路各级增益的求解方法;进而针对纯电阻网络组成的特殊AGC电路,简化了求解方法;给出了该类AGC电路的设计实例,测试结果满足35dB的干信比指标要求。分析方法不仅适用于导航接收机设计,还可推广应用于指导各类接收机的设计。     

消防设计审核范围探讨

根据我国现实情况和需要,结合相关法规规定要求,从维护法规的严肃性与权威性,保障消防监督执法的统一与规范出发,提出修改完善法规的原则性建议。     

A new importance sampling Monte Carlo method for a flow network reliability problem

The exact evaluation of the probability that the maximum st‐flow is greater than or equal to a fixed demand in a stochastic flow network is an NP‐hard problem. This limitation leads one to consider Monte Carlo alternatives. In this paper, we propose a new importance sampling Monte Carlo method. It is based on a recursive use of the state space decomposition methodology of Doulliez and Jamoulle during the simulation process. We show theoretically that the resulting estimator belongs to the variance‐reduction family and we give an upper bound on its variance. As shown by experimental tests, the new sampling principle offers, in many cases, substantial speedups with respect to a previous importance sampling based on the same decomposition procedure and its best performances are obtained when highly reliable networks are analyzed. © 2002 Wiley Periodicals, Inc. Naval Research Logistics 49: 204–228, 2002; DOI 10.1002/nav.10004     

利用极大值原理求解飞行器飞行区域

利用现代最优控制理论极大值原理 ,考虑给定约束条件下所有可能的控制方案 ,确定了一定时间内飞行器飞行区域。     

基于最大后验风险的多层Bayes方法

为了对指数型产品进行可靠性鉴定,首先给出了失效率的多层先验分布,然后从最大后验风险的角度,运用Bayes方法,制定出可靠性鉴定试验方案.按照此鉴定试验方案,缩短了试验时间,从而降低了鉴定试验所需的费用.     

зрлaнгa分布及其在保障性数据分析中的应用

首先对（?）分布的特点进行了分析,其次运用极大似然法对其分布参数t_0进行了估计,然后通过2个实例验证了这种分布的可行性和实用性,最后得出几点结论。SS