谈消防控制室的消防安全整体解决方案

消防控制室是建（构）筑物消防设施的控制、指挥、调度枢纽,是消防设施核心中的核心,直接决定能否尽早发现火灾、全面控制火灾、成功扑救火灾、组织迅速疏散。从设计、施工、使用三个方面系统阐述了消防控制室存在的常见问题及解决方案,以期科学、安全、合理地发挥消防控制室的各项功能。     

Halo轨道的航天器编队构型设计

针对不同干涉基线约束下的最优Halo轨道编队构型设计方法展开研究。以Richardson关于Halo轨道的三阶近似解析解为基础建立同一轨道上两航天器编队的相对运动学模型;以平动点为质心的旋转坐标系为基准构造与编队主航天器和观测目标相关的旋转坐标系,并在此坐标系中给出不同于二体问题的干涉基线计算方法;以满足基线约束下观测时间最长为目标给出最优编队构型设计方法。最后,以绕日-地L2点的Halo轨道为例对上述编队构型设计方法的有效性进行了仿真验证。     

防暴发射器身管长度优化研究

为解决某型防暴发射器身管设计不合理导致有效射程短的问题,以仿真设计的方法,运用Matlab计算软件对其进行了内弹道模拟仿真,获得了不同身管长度下该防暴发射器的膛压和速度曲线,确定了最优身管长度。然后利用ANsYs有限元分析软件,对延长身管后的模型进行了强度校核。仿真结果和实弹数据表明：防暴发射器身管长度设计合理,有效提高了其实际射程和作战效能,研究工作优化了防暴发射器的设计。     

基于UML的导弹伺服测试系统通用设计方法

分析了导弹伺服测试系统组成及功能,采用UML静态建模技术构建了导弹伺服测试系统设计的需求描述模型,运用动态建模方法建立了系统结构模型和行为模型,并以上述模型为基础,设计了导弹伺服测试系统通用软硬件结构。该方法优化了导弹伺服测试系统共性设计,并创建了特性模型架构和特化接口,有效提高了系统的设计效率和开发质量。     

机载相控阵雷达搜索模式辐射能量控制方法

机载相控阵雷达过高的辐射能量威胁了战斗机的生存能力。为了减少相控阵雷达搜索模式辐射能量,提出了基于辐射能量控制的搜索模型。将总能量消耗函数和检测概率相对误差作为目标函数,以平均功率、波束宽度、积累脉冲数以及脉冲重复间隔作为优化变量,选取非支配遗传排序算法对此模型进行优化。仿真结果表明,在同样检测概率情况下,提出的搜索方法可以有效控制雷达辐射能量,具有更好的射频隐身性能。     

The impact of operational decisions on the design of salesforce incentives

When facing high levels of overstock inventories, firms often push their salesforce to work harder than usual to attract more demand, and one way to achieve that is to offer attractive incentives. However, most research on the optimal design of salesforce incentives ignores this dependency and assumes that operational decisions of production/inventory management are separable from design of salesforce incentives. We investigate this dependency in the problem of joint salesforce incentive design and inventory/production control. We develop a dynamic Principal‐Agent model with both Moral Hazard and Adverse Selection in which the principal is strategic and risk‐neutral but the agent is myopic and risk‐averse. We find the optimal joint incentive design and inventory control strategy, and demonstrate the impact of operational decisions on the design of a compensation package. The optimal strategy is characterized by a menu of inventory‐dependent salesforce compensation contracts. We show that the optimal compensation package depends highly on the operational decisions; when inventory levels are high, (a) the firm offers a more attractive contract and (b) the contract is effective in inducing the salesforce to work harder than usual. In contrast, when inventory levels are low, the firm can offer a less attractive compensation package, but still expect the salesforce to work hard enough. In addition, we show that although the inventory/production management and the design of salesforce compensation package are highly correlated, information acquisition through contract design allows the firm to implement traditional inventory control policies: a market‐based state‐dependent policy (with a constant base‐stock level when the inventory is low) that makes use of the extracted market condition from the agent is optimal. This work appears to be the first article on operations that addresses the important interplay between inventory/production control and salesforce compensation decisions in a dynamic setting. Our findings shed light on the effective integration of these two significant aspects for the successful operation of a firm. © 2014 Wiley Periodicals, Inc. Naval Research Logistics 61: 320–340, 2014     

基于星架系统结构参数的卫星载荷减振方法

卫星工程中广泛采用的有效载荷支架结构可能会与卫星主体结构发生动力耦合,进而造成有效载荷响应显著放大。进一步将有效载荷支架与卫星主体结构考虑为一个整体系统(称为星架系统)。采用有限元方法建立某型卫星系统级动力学分析模型,从中提取结构参数建立集中参数模型,并针对结构参数进行单变量影响分析。结果表明:所建集中参数模型能够反映支架结构与卫星主体结构之间动力耦合规律,载荷响应对两者频率参数的敏感程度远高于其阻尼和质量参数,卫星结构设计阶段应重点考量主体结构和支架结构频率关系以优化卫星载荷的动力学环境。     

威胁环境生存突防优化策略分析

讨论了影响飞机作战生存性的主要因素,建立了生存概率模型。根据生存概率模型确立了威胁环境生存突防优化策略。最后,为了简化计算推导了实用危险性模型     

飞机战伤修理分析与实施

提出了飞机战伤修理分析的程序和方法,论述了战饬修理应具备的条件及实施步骤。同时也提出了我空军在战饬修理建设方面的一些建议。