机器人PTP控制曲线研究

本文根据点位控制机器人运动特点和其加速——匀速——减速三段控制方式,以及实时计算量的大小和所定义的点位控制机器人控制曲线参数——最大加速度系数、最大跃动系数,对点位控制机器人用控制曲线进行了系统、深入的分析,给出了一种变形sin加速度控制曲线,并在点位控制机器人上对其性能进行了验证。     

英国车辆电子学研究防御倡议(VERDI)述评

车辆电子学（ＶＥＴＲＯＮＩＣＳ）是近年来装甲车辆研究领域内兴起的一项意义深远的尖端技术。目前,最有影响的３个典型系统是美国的“标准陆军车辆电子系统体系结构（ＳＡＶＡ）”、英国的“车辆电子学研究防御倡议（ＶＥＲＤＩ）”及法国的全电子化主战坦克“勒克莱尔”。简单介绍了ＶＥＲＤＩ的研究历史,系统阐述了其第二研究阶段（ＶＥＲＤＩ－２）的改进方针、改进后的系统组成、设备配置、功能度及系统特征等。     

空间布置中的干涉性检查算法

本文提出一种新的干涉性检查算法:首先估计被测对象是否位于可能发生干涉的区域,若是,则再进一步检查它们之间是否接触或穿越等。算法简单明了,效率较高,适用面广,计算机运行结果证实了算法的正确性和可靠性。     

潜艇承载力分析和动力抗沉操纵方法研究

在分析潜艇受力的基础上,根据潜艇的操纵规则,给出承载力的计算方法,分析了影响潜艇承载力的因素,设计了一套用于指导潜艇动力抗沉操纵的承载力图谱.以某一假想潜艇为例,说明了承载力图谱的绘制和使用方法.     

浅议陆军合成旅装备一体化联合检验

近年来,装备试验深入推进。作为装备试验领域的最高形式,装备一体化联合检验已经成为陆军合成旅装备试验的新趋势和新常态。本文从装备一体化联合检验的概念入手,简要阐述了以作战效能、作战适用性、体系适用性和在役适用性为主的“一能三性”,从装备体系效能的联合检验、装备体系运用的具体检验和陆军合成旅的综合检验三个方面深入理解和认识装备一体化联合检验,提出了立足联合作战、立足贴近实战、紧盯短板弱项、聚焦摸清底数等四个需要重点关注的问题,以为陆军合成旅装备一体化联合检验的深入开展提供理论参考和借鉴。     

Supercritical carbon dioxide as a new working medium for pneumatic launch: A theoretical study

Compared with the conventionally gaseous or liquid working media, the specific internal energy of supercritical carbon dioxide (SCD) is higher at the same temperature and pressure, and the critical temperature of carbon dioxide is close to room temperature, making SCD a potential new working medium for pneumatic launch. To analyze the feasibility of this conception, an analytical model of a pneumatic catapult is established on basis of the conservations of mass and energy. The model consists of a high-pressure chamber and a low-pressure chamber connected by multiple valves, and there is a movable piston in the low-pressure chamber that can push an aircraft to accelerate. The effects of the launch readiness state of SCD in the high-pressure chamber, the initial volume of the low-pressure chamber and the valve control on the movement of the aircraft are analyzed. It is found that there is a restrictive relation between the temperature and pressure of the launch readiness state of SCD, i.e., there is a maximum allowable launch readiness pressure when the launch readiness temperature is fixed. If this restrictive relation is not satisfied, the working medium in the low-pressure chamber will drop to its triple point within a few milliseconds, leading to a launch failure. Owing to this restrictive relation, there is an optimal launch readiness state of SCD with the highest working capacity for any allowable launch readiness temperature. The pressure of the low-pressure chamber will decrease significantly as the initial volume increases, leading to a decreased acceleration of the aircraft. The ac-celeration can be controlled below a critical value by a designed sequential blasting technique of multiple valves. The calculated results show that a 500 kg aircraft can be accelerated from 0 to 58 m/s in 0.9 s with 36 kg of carbon dioxide. This research provides a new technique for the controllable cold launch of an aircraft.     

Disruption management in production planning

We study the problem of recovering a production plan after a disruption, where the disruption may be caused by incidents such as power failure, market change, machine breakdown, supply shortage, worker no‐show, and others. The new recovery plan we seek after has to not only suit the changed environment brought about by the disruption, but also be close to the initial plan so as not to cause too much customer unsatisfaction or inconvenience for current‐stage and downstream operations. For the general‐cost case, we propose a dynamic programming method for the problem. For the convex‐cost case, a general problem which involves both cost and demand disruptions can be solved by considering the cost disruption first and then the demand disruption. We find that a pure demand disruption is easy to handle; and for a pure cost disruption, we propose a greedy method which is provably efficient. Our computational studies also reveal insights that will be helpful to managing disruptions in production planning. © 2005 Wiley Periodicals, Inc. Naval Research Logistics, 2005.     

A concave‐cost production planning problem with remanufacturing options

We focus on the concave‐cost version of a production planning problem where a manufacturer can meet demand by either producing new items or by remanufacturing used items. Unprocessed used items are disposed. We show the NP‐hardness of the problem even when all the costs are stationary. Utilizing the special structure of the extreme‐point optimal solutions for the minimum concave‐cost problem with a network flow type feasible region, we develop a polynomial‐time heuristic for the problem. Our computational study indicates that the heuristic is a very efficient way to solve the problem as far as solution speed and quality are concerned. © 2005 Wiley Periodicals, Inc. Naval Research Logistics, 2005     

钢管初应力对方钢管混凝土构件性能的影响研究

在14根方钢管混凝土构件试验的基础上,分析了初应力系数、荷载偏心率、混凝土强度、试件长细比等因素对承载力的影响,给出了钢管初应力对方钢管混凝土压弯构件承载力的影响系数,采用ANSYS有限元分析程序进行了非线性全过程分析.     

论校园文化建设的内容与规划——基于华山中学校园文化建设活动的系列思考之二

开展校园文化建设必须以马克思主义文化观作为指导思想,在此基础上,要全面了解校园文化建设的内容,进行科学规划,稳步实施,才能收到成效。本文结合华山中学的具体实践,阐述了对校园文化建设工作的认识,并且提出以校园文化建设为目标的教育形式才可以称得上是全面教育,它比侧重传授知识的教育模式更加接近教育的本质规律,更加反映人性发展的需要,也更加符合人类社会发展的方向。