Dynamic lot‐sizing model with production time windows

We consider a dynamic lot‐sizing model with production time windows where each of n demands has earliest and latest production due dates and it must be satisfied during the given time window. For the case of nonspeculative cost structure, an O(nlogn) time procedure is developed and it is shown to run in O(n) when demands come in the order of latest production due dates. When the cost structure is somewhat general fixed plus linear that allows speculative motive, an optimal procedure with O(T⁴) is proposed where T is the length of a planning horizon. Finally, for the most general concave production cost structure, an optimal procedure with O(T⁵) is designed. © 2007 Wiley Periodicals, Inc. Naval Research Logistics, 2007     

Exact expected values of variance estimators for simulation

We formulate exact expressions for the expected values of selected estimators of the variance parameter (that is, the sum of covariances at all lags) of a steady‐state simulation output process. Given in terms of the autocovariance function of the process, these expressions are derived for variance estimators based on the simulation analysis methods of nonoverlapping batch means, overlapping batch means, and standardized time series. Comparing estimator performance in a first‐order autoregressive process and the M/M/1 queue‐waiting‐time process, we find that certain standardized time series estimators outperform their competitors as the sample size becomes large. © 2007 Wiley Periodicals, Inc. Naval Research Logistics, 2007     

A produce‐to‐stock system with advance demand information and secondary customers

We consider a manufacturer (i.e., a capacitated supplier) that produces to stock and has two classes of customers. The primary customer places orders at regular intervals of time for a random quantity, while the secondary customers request a single item at random times. At a predetermined time the manufacturer receives advance demand information regarding the order size of the primary customer. If the manufacturer is not able to fill the primary customer's demand, there is a penalty. On the other hand, serving the secondary customers results in additional profit; however, the manufacturer can refuse to serve the secondary customers in order to reserve inventory for the primary customer. We characterize the manufacturer's optimal production and stock reservation policies that maximize the manufacturer's discounted profit and the average profit per unit time. We show that these policies are threshold‐type policies, and these thresholds are monotone with respect to the primary customer's order size. Using a numerical study we provide insights into how the value of information is affected by the relative demand size of the primary and secondary customers. © 2007 Wiley Periodicals, Inc. Naval Research Logistics, 2007     

空靶脱靶量测量方法研究

通过对正弦波、三角波和锯齿波三种调频信号差频测距方法的深入研究,认为三种波形调频差频频谱是连续的.正弦波和三角波调频时,差频有周期性不规则区,测距出现模糊,而锯齿波调频差频规律性强,测距清晰,并给出了锯齿波调频测距的一般表达式,理论上证明了锯齿波调频差频测距的连续性.在研究空靶脱靶量测量中,提出了利用锯齿波调频差频完成空靶脱靶量测量方法,探讨了系统的设计与实现.     

Ag2O 添加的YBa2 Cu3O7-δ超导材料的超导性能

用固态反应法按分子式ＹＢａ２Ｃｕ２．７Ａｇ０．３Ｏ７－δ（简称ＹＢＣＡＯ）制备了样品，利用Ｘ射线衍射，Ｒ－Ｔ曲线及扫描电镜ＳＥＭ研究了Ａｇ对于ＹＢＣＯ超导性能的影响。实验结果表明：晶粒得以细化，ＹＢＣＯ超导性能的稳定性有所增强。本文对结果进行了讨论。     

舰艇防空火力规划与调度方法研究

根据舰艇防空武器拦截过程的时间连续性和拦截效果的不确定性特点,提出了智能规划和优化调度相结合的舰艇防空计划生成方法。在规划阶段,先用智能规划描述语言PDDL对舰艇防空问题进行建模;针对新的来袭目标或观察的拦截结果,利用智能规划的高效行动推理能力,快速生成可能的备选行动方案;在优化调度阶段,对已生成的备选方案的行动系列进行时间、资源冲突处理,并计算选择出当前最佳拦截方案。与现有的采用离散化处理的武器-目标分配方法相比,该规划与调度过程充分体现了拦截过程的连续性,拦截效果的不确定性,拦截过程中的武器协同,以及最佳拦截时机的选择等,更好地描述了舰艇防空的实际过程。最后,通过蒙特卡罗仿真试验,验证了算法的有效性,为舰艇的自动化防空提供了一种新的解决办法。     

拟带宽 Toeplitz 系统的秩 1 修正算法

本文以带宽Ｔｏｅｐｌｉｔｚ系统的快速并行解法为基础,通过建立秩１的修正格式讨论了拟带宽Ｔｏｅｐｌｉｔｚ系统的一种快速并行算法,其串行运算量为９ｎｈ＋Ｏ（ｈ）．设ｐ为处理机台数,当ｐ≤ｎ时,并行运算量为　;当ｐ＝３ｎ时,运算量为２ｈ￣２ｌｏｇ２ｎ＋Ｏ（１）,其中ｈ表示拟带宽宽度。     

磁性微粉/聚乙烯复合材料的电磁特性

研究了磁性微粉的物相组成及其与聚乙烯相复合制成的吸波材料在８． ２～１２． ４ＧＨｚ 频段内的电磁特性。结果表明： 复合材料中聚乙烯的加入量对电磁特性在上述频段内各频率范围影响程度不同； 磁性微粉中聚碳硅烷量为２０％ 时， 反射衰减大于６ｄＢ对应的频带宽度为２ＧＨｚ。     

考虑有损伤测量条件下的设备剩余寿命的建模分析

在有损测量的情况下,仅从退化数据本身出发所建的模型不能反映设备的真实退化过程.尤其在测量导致的设备性能退化量不可忽略时,不考虑测量耗损量将不能有效进行预测和评估.为解决这个问题,首先基于维纳过程建立有损测量的设备退化过程,进一步给出了相应模型的参数估计方法和基于贝叶斯理论的设备剩余寿命的实时更新方法,最后通过一个仿真示...     

稀薄流高超声速飞行器气动加热耦合计算

针对稀薄流域高超声速飞行器的气动加热问题,开展耦合数值计算研究。通过引入牛顿冷却定律,将直接模拟蒙特卡洛数值模拟方法与结构传热计算方法相结合,设计一种可对全机外形进行气动热和结构传热计算的高效松耦合方法,实现飞行器防热层结构材料温度分布特性的数值模拟。在以钝锥外形为例对直接模拟蒙特卡洛数值模拟程序进行验证的基础上,采用该方法对X37B轨道飞行器外形长时加热与结构传热过程进行数值模拟,给出结构温度及热流密度随飞行时间的变化规律。研究结果表明,设计的耦合计算方法能够模拟稀薄流域高超声速飞行器的气动加热及结构传热耦合过程,可为该类飞行器的气动热分析及热防护设计提供技术支持。