设备的一种计划维修策略

本文根据设备在全寿命内有事后修理、计划修理和最后报废的实际情况,以全寿命内单位时间的更新维修期望费用最少为目标函数,建立一种数学模型,寻求设备在全寿命内最佳计划修理次数N和最佳的一组计划维修时间间隔集T。     

火控系统最佳采样率问题的研究

先从滤波器和信号的频域特性出发给出了滤波器在频域的采样率匹配原则。第二部分从滤波器预测误差最小的原则出发导出了一组求解最佳采样时间的方程,并给出部分计算结果。第三部分提出了速度平滑处理法,解决了提高采样率引起的速度估计误差增大的矛盾。随后给出了典型航路下,综合各影响因素的模拟跟踪结果,并与“×型”指挥仪的跟踪结果作了分析对比。最后提出了针对不同空中目标的最佳采样率的建议     

载人飞船返回段的最优控制

本文介绍空间飞船再入段最优制导方法。纵向制导采用二次型性能指标最优的线性系统,得到最优控制规律。侧向制导利用庞特里亚金最小原理,得到最优开关曲线。结果表明,这些控制规律优于Rodney C.所介绍的制导方法。     

基于灰色时序的完整性规范技术

计算机系统的完整性安全策略模型与规范问题，是计算机安全研究中最重要的课题之一。已有的研究结果离实际应用还相差太远，例如Ｃｌａｒｋ－Ｗｉｌｓｏｎ完整性模型只是提出了一个框架。本文呈现了我们构造的形式化灰色时序安全策略规范语言（ＧＴＳＬ）。ＧＴＳＬ的理论基础是灰色系统理论和时序规范语言ＬＯ－ＴＯＳ理论。由于它在完整性规范能力、完整性验证过程的构造与表示、责任分离合理性测试等一系列技术方面的完善与创新，使得ＧＴＳＬ成为真正能够实际使用的完整性安全策略规范语言。     

On efficient algorithms for finding efficient salvo policies

We consider the salvo policy problem, in which there are k moments, called salvos, at which we can fire multiple missiles simultaneously at an incoming object. Each salvo is characterized by a probability p_i: the hit probability of a single missile. After each salvo, we can assess whether the incoming object is still active. If it is, we fire the missiles assigned to the next salvo. In the salvo policy problem, the goal is to assign at most n missiles to salvos in order to minimize the expected number of missiles used. We consider three problem versions. In Gould's version, we have to assign all n missiles to salvos. In the Big Bomb version, a cost of B is incurred when all salvo's are unsuccessful. Finally, we consider the Quota version in which the kill probability should exceed some quota Q. We discuss the computational complexity and the approximability of these problem versions. In particular, we show that Gould's version and the Big Bomb version admit pseudopolynomial time exact algorithms and fully polynomial time approximation schemes. We also present an iterative approximation algorithm for the Quota version, and show that a related problem is NP-complete.     

利用径向力平衡飞行控制的航天器高精度轨道捕获方法

为实现对探测器轨道形状与高度的精准调整,提出一种径向力平衡飞行的航天器连续推力控制新方法。建立连续推力平衡飞行的动力学极坐标模型,并推导出特殊条件下的解析轨道解,进一步分析边值条件,给出连续推力的控制律。利用这一平衡飞行控制理论,构建轨道捕获的最优控制策略。考虑推力器的推力水平,通过一次或多次的控制过程,实现对轨道形状、轨道高度及轨道相位的综合调整。数值仿真表明:利用平衡飞行的轨道控制方法,配置微小推力器的空间引力波探测器可以实现高精度的轨道捕获;该方法具有控制过程可解析、计算量小、简便、实用等特点。     

辐射传热时活塞式气缸中加热气体的最大膨胀功

对热辐射传热定律q∝Δ(T4)下,给定初态内能、体积,末态体积以及过程时间时,加热气体膨胀的最优构型进行了研究,利用最优控制理论得出最大膨胀功输出时膨胀的最优构型由两个瞬时绝热分支和一个E-L分支组成的结论.给出了各分支之间转换点参数的求解方法及最优构型的数值算例,最后将线性唯象传热定律、牛顿传热定律、平方传热定律、立方传热定律和辐射传热定律下加热气体膨胀的最优构型进行了比较.结果显示,随着传热指数的增加,理想气体的内能呈现出明显的整体增加趋势,而体积则呈现出明显的整体减小趋势.     

基于最大故障特征信息熵的测试点优化设计

为解决故障诊断和可测试性设计中普遍存在的测试点优化问题,以相关性矩阵模型为基础,建立了最大故障特征信息熵的优化准则,给出了相应的测试点优化设计方法。应用实例表明：该方法是可行的、正确的,能为武器装备的故障诊断和可测试性设计提供有力的支持。     

Dynamic inventory management with cash flow constraints

In this article, we consider a classic dynamic inventory control problem of a self‐financing retailer who periodically replenishes its stock from a supplier and sells it to the market. The replenishment decisions of the retailer are constrained by cash flow, which is updated periodically following purchasing and sales in each period. Excess demand in each period is lost when insufficient inventory is in stock. The retailer's objective is to maximize its expected terminal wealth at the end of the planning horizon. We characterize the optimal inventory control policy and present a simple algorithm for computing the optimal policies for each period. Conditions are identified under which the optimal control policies are identical across periods. We also present comparative statics results on the optimal control policy. © 2008 Wiley Periodicals, Inc. Naval Research Logistics 2008     

What Is Known About Defence Research And Development Spill-Overs?

This article surveys the body of available evidence regarding the spill-over effects of defence R&D. It reviews the routes through which defence R&D spills over to the economy with positive externalities – in terms of new products, technologies or processes; the barriers that impede or block such a process; potential negative repercussions, and the measure of such effects. The main conclusion is that the uncertainty of these effects, and the inaccurate appraisal of their value, hardly supports informed decisions concerning defence R&D policies.