浅谈现代远程教育对武警院校教学的深远影响

武警院校拥有丰富的教育资源，依托武警部队日益健全的内部网络系统，大力开展现代远程教育，能够更加紧密院校与部队的联系，及时了解部队的需求，制定出更加符合部队实际的课程体系，更大限度发挥现有教学资源的效益。由于远程教育具有方便快捷，受时间、空间局限小的特性，弥补了由于武警部队点多、线长、面广，分布相对分散，导致部队官兵学习时间不固定、人员难以集中等不便的问题，为武警部队官兵获取文化知识，学习科学技术提供了新的途径。     

基于模型跟踪变结构控制的飞行重构控制律设计

提出一种基于模型跟踪变结构控制的飞行重构控制律的设计方法.利用该方法能实现受控对象对理想模型较高精度的跟踪,使重构飞行控制系统具有较好的控制性能.首先设计了一个比例-积分滑模面以确保消除稳态误差,采用极点配置技术使滑模具有良好的动态品质,其次利用饱和控制技术来减少变结构控制引起的抖振现象,最后以某型飞机纵向飞行控制系统为例进行了相应的数字仿真.结果表明重构系统不仅实现了无抖振模型跟踪,而且还具有较强的鲁棒性.     

Optimal outbound dispatch policies: Modeling inventory and cargo capacity

In this paper, we present an optimization model for coordinating inventory and transportation decisions at an outbound distribution warehouse that serves a group of customers located in a given market area. For the practical problems which motivated this paper, the warehouse is operated by a third party logistics provider. However, the models developed here may be applicable in a more general context where outbound distribution is managed by another supply chain member, e.g., a manufacturer. We consider the case where the aggregate demand of the market area is constant and known per period (e.g., per day). Under an immediate delivery policy, an outbound shipment is released each time a demand is realized (e.g., on a daily basis). On the other hand, if these shipments are consolidated over time, then larger (hence more economical) outbound freight quantities can be dispatched. In this case, the physical inventory requirements at the third party warehouse (TPW) are determined by the consolidated freight quantities. Thus, stock replenishment and outbound shipment release policies should be coordinated. By optimizing inventory and freight consolidation decisions simultaneously, we compute the parameters of an integrated inventory/outbound transportation policy. These parameters determine: (i) how often to dispatch a truck so that transportation scale economies are realized and timely delivery requirements are met, and (ii) how often, and in what quantities, the stock should be replenished at the TPW. We prove that the optimal shipment release timing policy is nonstationary, and we present algorithms for computing the policy parameters for both the uncapacitated and finite cargo capacity problems. The model presented in this study is considerably different from the existing inventory/transportation models in the literature. The classical inventory literature assumes that demands should be satisfied as they arrive so that outbound shipment costs are sunk costs, or else these costs are covered by the customer. Hence, the classical literature does not model outbound transportation costs. However, if a freight consolidation policy is in place then the outbound transportation costs can no longer be ignored in optimization. Relying on this observation, this paper models outbound transportation costs, freight consolidation decisions, and cargo capacity constraints explicitly. © 2002 Wiley Periodicals, Inc. Naval Research Logistics 49: 531–556, 2002; Published online in Wiley InterScience (www.interscience.wiley.com). DOI 10.1002/nav.10030     

MUOS网络管理与控制技术的研究

介绍了美军移动用户目标系统MUOS(Mobile User Objective System),分析和总结了该系统下网络管理体系结构和运行机制,并就其实现中的关键技术进行了深入研究,得到了一些对我国有借鉴意义的结论。     

公安边防部门刑事侦查权的取得与完善

公安边防部门取得刑事侦查权，是侦查体制改革的结果。但在边防管辖和查办案件的种类、边防海警刑事办案权的实现、边防检查站查获的刑事案件的管辖、公安边防部门侦查主体资格的完善等方面，还应继续改革．使边防部门刑事侦查机制不断完善。     

火灾自动报警器及消防联动控制设计中常见问题浅析

在建筑消防设计审核、验收和工程实践中发现了火灾自动报警器及消防联动控制系统存在的一些问题，依据国家有关规范要求，提出了设计中应该注意的事项。     

脉冲等离子体推力器羽流的粒子模拟

目前微小卫星正在积极地发展中,脉冲等离子体推力器是其推进系统的一个重要发展方向,为了能够将PPT成功地运用于空间,需对其羽流进行研究.将DSMC(Direct Simulation Monte-Carlo)/PIC(Particle in Cell)流体混合算法与一维MHD放电模型相结合,一体化模拟NASA Glenn PPT羽流,对不同出口偏转角的羽流场进行模拟,并与实验结果进行了比较.计算结果显示引入出口速度的偏转角提高了模型的羽流扩散能力,羽流的扩散角是影响羽流的一个主要因素.     

装备维修性增长及其基本过程研究

为了解决当前装备的维修性问题，揭示维修性发展的一般规律，进行了维修性增长的研究。首先阐明了装备维修性形成与演变的一般规律，继而提出了维修性增长的概念，重点研究了维修性增长的内涵与增长的一般过程，最后对解决增长问题所需的模型进行了分类，为增长技术的深入研究奠定了基础。     

通用扩张状态观测器鲁棒飞行控制方法

针对存在参数不确定、外界干扰与测量噪声情况下飞行控制问题，提出一种基于通用扩张状态观测器的鲁棒飞行控制方法。首先基于状态相关的Riccati方程（SDRE）控制方法，对飞行器俯仰通道非线性模型进行扩展线性化；而后引入基于通用扩张状态观测器的控制方法，设计干扰补偿增益，实现对外界干扰的估计与补偿；最后通过在线解算状态相关矩阵及代数黎卡提方程，得出状态反馈增益与干扰补偿增益，实现对飞行器期望攻角的跟踪控制。通过与已有方法进行对比，验证了本文所提方法不仅对系统模型不确定性与外界干扰具有较强鲁棒性，而且在较大测量噪声情况下，其依然能够保证良好的跟踪控制效果，具有较强的工程应用价值。