带落角约束的再入机动弹头的复合导引律

针对再入机动弹头垂直打击目标的要求,研究了具有末端落角约束的复合导引律.该导引律包括俯冲平面内的制导方程和转弯平面内的制导方程,通过在最优导引律的基础上引入滑模变结构控制,增强导引律的鲁棒性.为了减小控制量的抖振和能量损耗,提出了采用RBF(径向基函数)神经网络自适应调节切换项增益的方案,数学仿真验证了该方案的有效性.仿真结果还表明,与最优导引律相比,复合导引律在外界干扰的影响下仍能保持较高的制导精度.     

非线性积分方程的周期解

以（Cg,｜.｜g）为相空间,研究具有无限时滞非线性积分方程周期解的存在性,利用Schauder-Tychonov不动点定理证明方程解的g一致有界性和g一致最终有界性蕴含周期解的存在性。     

Designing a screening experiment for highly reliable products

Within a reasonable life‐testing time, how to improve the reliability of highly reliable products is one of the great challenges to today's manufacturers. By using a resolution III experiment together with degradation test, Tseng, Hamada, and Chiao (1995) presented an interesting case study of improving the reliability of fluorescent lamps. However, in conducting such an experiment, they did not address the problem of how to choose the optimal settings of variables, such as sample size, inspection frequency, and termination time for each run, which are influential to the correct identification of significant factors and the experimental cost. Assuming that the product's degradation paths satisfy Wiener processes, this paper proposes a systematic approach to the aforementioned problem. First, an intuitively appealing identification rule is proposed. Next, under the constraints of a minimum probability of correct decision and a maximum probability of incorrect decision of the proposed identification rule, the optimum test plan (including the determinations of inspection frequency, sample size, and termination time for each run) can be obtained by minimizing the total experimental cost. An example is provided to illustrate the proposed method. © 2002 Wiley Periodicals, Inc. Naval Research Logistics 49: 514–526, 2002; Published online in Wiley InterScience (www.interscience.wiley.com). DOI 10.1002/nav.10024     

Column generation for stochastic green telecommunication network planning with switchable base stations

We present the green telecommunication network planning problem with switchable base stations, where the location and configuration of the base stations are optimized, while taking into account uncertainty and variability of demand. The problem is formulated as a two‐stage stochastic program under demand uncertainty with integers in both stages. Since solving the presented problem is computationally challenging, we develop the corresponding Dantzig‐Wolfe reformulation and propose a solution approach based on column generation. Comprehensive computational results are provided for instances of varying characteristics. The results show that the joint location and dynamic switching of base stations leads to significant savings in terms of energy cost. Up to 30% reduction in power consumption cost is achieved while still serving all users. In certain cases, allowing dynamic configurations leads to more installed base stations and higher user coverage, while having lower total energy consumption. The Dantzig‐Wolfe reformulation provides solutions with a tight LP‐gap eliminating the need for a full branch‐and‐price scheme. Furthermore, the proposed column generation solution approach is computationally efficient and outperforms CPLEX on the majority of the tested instances. © 2016 Wiley Periodicals, Inc. Naval Research Logistics 63: 351–366, 2016     

电子战条件下飞机敏感性分析及其减缩技术

介绍了电子战和飞机生存力及敏感性的内涵,构建了飞机敏感性量化评价指标层次体系。定性分析了电子干扰对雷达探测概率和导弹脱靶距离标准差的影响,并以算例说明了干扰效能的增大会引起导弹制导精度的降低和脱靶距离的增大,从而得出:电子干扰对飞机的敏感性和生存概率有重要的影响。引入了干扰效能因子的概念,并分析了将干信比J/S作为一种干扰效能因子考虑的可行性及优点。最后给出了降低飞机敏感性的电子战措施。     

再入弹道参数自适应估计

本文研究再入弹道参数的自适应估计。所采用的方法对动力学模型噪声的未知统计特性进行补偿,并对状态参数与测量设备的系统误差交叉进行估计。仿真结果表明,无论是状态参数的估计还是测量系统误差的估计,都具有较高的精度。     

汇编语言动态分析工具中的程序插装技术

根据8086/8088语言的结构化特点,提出了程序插装的概念及其实现方法,并基于插装研制出一种动态分析工具,从而实现了对程序分支及语句的自动测试功能.     

导弹飞行试验外测系统误差的估计

在导弹飞行试验中,遥外测数据是进行精度和可靠性分析的依据。通常假定外测误差服从零均值正态分布,而在实际测量中,外测参数有可能带有系统误差,它的存在对飞行轨道和落点信息的获取都具有不利的影响。在一定的模型假设下,本文获得了外测系统误差的估计,并对一些仿真结果进行了初步分析。     

模糊综合评判在雷达接收机等级评定中的应用

为消除技术等级评定中主观因素的影响,将多级模糊综合评判的方法运用于接收机的技术等级评定中。对雷达接收机的技术性能指标进行了层次分类,采用了一种以测试数据为基础的针对每一个因素的单因素评判方法,并以某型雷达接收机为例,给出其技术等级模糊综合评判的详细求解过程。     

高效率机动部署航空武器靶场关键技术和应用

为用户设计了一个航空武器试验靶场,具备空空、空地和地空导弹试验能力,可机动部署,具有易于运行和运维代价低的特点。靶场由载机遥测系统、测量雷达、光电跟踪系统、微波和光纤通信系统、靶机遥测站、指挥控制等6个子系统构成;指挥控制子系统之外的5个子系统均使用国产成熟产品。在总体方案和指挥控制子系统设计中,对互联集成方案、机动部署、试验航线设计和发布、自动化领航、自动化指挥决策等5项关键技术进行了着重优化。在实际应用中,全靶场运行仅需20多成员(不含飞行和机场机务人员),3天内完成新试验场部署和联调,对作战部队飞行员进行5架次航线训练后即进行实弹试验,2天内完成多发中程拦截和近距格斗空空导弹试验。