雷达天线俯仰控制及威力显示系统的设计

介绍现有雷达天线俯仰控制及显示系统的缺点 ,提出采用单片机控制、液晶显示威力图的方式改造天线俯仰系统。同时给出了系统硬件设计和软件设计。     

When to commit in a serial supply chain with forecast updating

Negotiations between an end product manufacturer and a parts supplier often revolve around two main issues: the supplier's price and the length of time the manufacturer is contractually held to its order quantity, commonly termed the “commitment time frame.” Because actual demand is unknown, the specification of the commitment time frame determines how the demand risk is shared among the members of the supply chain. Casual observation indicates that most manufacturers prefer to delay commitments as long as possible while suppliers prefer early commitments. In this paper, we investigate whether these goals are always in the firm's best interest. In particular, we find that the manufacturer may sometimes be better off with a contract that requires an early commitment to its order quantity, before the supplier commits resources and the supplier may sometimes be better off with a delayed commitment. We also find that the preferred commitment time frame depends upon which member of the supply chain has the power to set their exchange price. © 2003 Wiley Periodicals, Inc. Naval Research Logistics, 2003     

A specially structured nonlinear integer resource allocation problem

We present an algorithm for solving a specially structured nonlinear integer resource allocation problem. This problem was motivated by a capacity planning study done at a large Health Maintenance Organization in Texas. Specifically, we focus on a class of nonlinear resource allocation problems that involve the minimization of a convex function over one general convex constraint, a set of block diagonal convex constraints, and bounds on the integer variables. The continuous variable problem is also considered. The continuous problem is solved by taking advantage of the structure of the Karush‐Kuhn‐Tucker (KKT) conditions. This method for solving the continuous problem is then incorporated in a branch and bound algorithm to solve the integer problem. Various reoptimization results, multiplier bounding results, and heuristics are used to improve the efficiency of the algorithms. We show how the algorithms can be extended to obtain a globally optimal solution to the nonconvex version of the problem. We further show that the methods can be applied to problems in production planning and financial optimization. Extensive computational testing of the algorithms is reported for a variety of applications on continuous problems with up to 1,000,000 variables and integer problems with up to 1000 variables. © 2003 Wiley Periodicals, Inc. Naval Research Logistics 50: 770–792, 2003.     

核动力装置的(火用)分析

针对压水堆、沸水堆、气冷堆、钠冷堆核动力装置的实际过程,建立了最简单的热动力学模型.利用热力学第二定律建立的火用分析方法,对核动力装置中主要的热量传递、作功与受功过程的不可逆性进行了分析.文中以A型和B型电站压水堆核动力装置为实例进行的火用损失与火用效率的对比计算表明反应堆内裂变能从裂变碎片到燃料的传递过程是整个核动力力装置火用损失最大的地方,其次是堆内燃料元件导热过程,然后依次是汽轮机、蒸发器、冷凝器、管路、泵.而火用效率最低的地方是冷凝器,其次是汽轮机、堆内燃料元件、蒸发器.     

非接触爆炸作用下舰船动力系统生命力的研究方法

分析非接触爆炸作用下舰船动力系统中主要设备的破坏模式 ,建立了动力设备的冲击响应模式 ,并给出了在非接触爆炸作用下用于舰船动力系统生命力评估的系统破坏概率计算机仿真计算方法。     

基于LUT的射频预失真技术

分析了当前文献中几种主要的预失真结构,发现这些预失真结构均不适用于多通道宽频带短波通信中高功率放大器的线性化.提出了一种新的数字射频预失真方案,该方案能够完全适应短波宽频通信的高精度、多通道、宽频带的要求,而且不需要使用射频非线性有源器件.仿真结果表明,在短波通信系统采用这种方案,可以在很大程度上改善功率放大器的线性度.     

坦克炮火力威力评价的多指标灰色关联决策模型

为了对坦克炮火力威力进行评估,提出一种新的解决方法.针对坦克炮火力威力评价中需要进行多属性、多指标决策的特点,利用在"奖优罚劣"原则基础上建立的[-1,1]线性变换算子,寻求决策方案的正、负理想方案,计算评价方案与正、负理想方案的关联度,建立了坦克炮火力威力评价的灰色关联度决策模型.计算实例的结果表明,该模型计算简捷、分辨程度较高、稳定性也好,可应用于坦克炮火力威力评价.     

用于电压岛式功耗管理的无运放结构高精度电流采样电路

电压岛式的功耗管理在大规模SoC芯片中的应用越来越广泛,由于负载电流是反映功耗最直接的物理量,因此对负载电流的实时、精确采样是对功耗进行精确管理和控制的基础,而低压大电流又是当前大规模芯片的基本特征.在分析了几种常用的电流采样技术的基础之上,提出了一种基于电流镜采样的高精度的电流采样方案,适合于低电源电压供电,并且不需要使用运算放大器,结构简单.基于0.18μm CMOS工艺实现了该电流采样电路,各种条件下的版图模拟结果表明,对于60～1300mA的负载,该电路的采样精度最高可达99.1%,并且自身功耗不超过4mW.利用该电流采样电路,可以对负载电流进行实时有效的高精度侦测,用以作为功耗管理的依据.     

炮兵火力任务分配的优化模型

现代作战,参战兵种多,炮兵的火力单位和类型更为复杂,不同的火力单位具有不同的毁伤效果,如何用最小的代价取得最大的军事效益,是一种火力任务分配的优化问题.根据不同炮种和目标的特点,建立在一定约束条件下的炮兵火力任务分配模型,并将其转化为指派问题,运用匈牙利算法求解,达到优化分配火力任务的目的.通过仿真计算证明这是辅助指挥员进行射击决策的一种有效手段,为作战指挥理论提供了一种新的数学模型.     

多操纵面战斗机飞行控制系统设计

现代多操纵面战斗机飞行控制系统多采用非线性控制方法进行设计,其中逆系统方法具有物理概念清晰、参数对应明确、无不确定性算法、容易结合传统经验等优点,易于工程实现.将该方法应用于多操纵面战斗机的基本控制律设计,使用多层简化设计,改进了多操纵面的控制分配策略,并针对某型多操纵面战斗机六自由度模型进行数字仿真,效果良好.