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991.
992.
高层体系结构HLA建立一个通用的仿真框架,以解决不同仿真器、模型之间的互操作及仿真组件的可重用性问题.针对当前空防对抗的主要特点,在地空导弹拦截的数学模型的基础上,利用HLA技术框架,详细地叙述了地空导弹拦截仿真系统的开发过程.仿真试验表明该系统能有效评估地空导弹火力单元对来袭目标的有效抗击效率和火力范围,为地空导弹火力单元的部署和作战效能的改进提供辅助决策手段. 相似文献
993.
994.
针对协同性联合作战向一体化联合作战转变对作战指挥产生的影响,在正确定位指挥信息流通体系的基础上,从一体化联合作战的本质特征及对指挥信息流通体系的影响出发,设计了基本作战单元指挥信息输入、输出模型,并通过将作战体系区分为四类模块,得出了指挥信息流通体系的逻辑结构. 相似文献
995.
2009年,Tu和Deng在一个组合猜想成立的基础上,构造了同时具有最优代数免疫性、最优代数次数和高非线性度的一类偶数元布尔函数.这类函数被称为Tu-Deng函数.基于同一猜想,Tu和Deng又构造了同时具有次最优代数免疫性、最优代数次数和较高非线性度的一类偶数元的l -阶弹性函数.通过研究由Tu-Deng函数导出的两个布尔函数的级联的密码学性质,在Tu-Deng猜想成立的基础上,给出一类奇数元的1 -阶弹性布尔函数.这类函数同时具有次最优代数免疫性、最优代数次数和较高非线性度. 相似文献
996.
Consider a simulation experiment consisting of v independent vector replications across k systems, where in any given replication one system is selected as the best performer (i.e., it wins). Each system has an unknown constant probability of winning in any replication and the numbers of wins for the individual systems follow a multinomial distribution. The classical multinomial selection procedure of Bechhofer, Elmaghraby, and Morse (Procedure BEM) prescribes a minimum number of replications, denoted as v*, so that the probability of correctly selecting the true best system (PCS) meets or exceeds a prespecified probability. Assuming that larger is better, Procedure BEM selects as best the system having the largest value of the performance measure in more replications than any other system. We use these same v* replications across k systems to form (v*)k pseudoreplications that contain one observation from each system, and develop Procedure AVC (All Vector Comparisons) to achieve a higher PCS than with Procedure BEM. For specific small-sample cases and via a large-sample approximation we show that the PCS with Procedure AVC exceeds the PCS with Procedure BEM. We also show that with Procedure AVC we achieve a given PCS with a smaller v than the v* required with Procedure BEM. © 1998 John Wiley & Sons, Inc. Naval Research Logistics 45: 459–482, 1998 相似文献
997.
Statistical estimation plays an important role in locating a target in space, a task that has important applications in many areas. However, theoretical measures on the quality of various estimators reported in the literature have been difficult to obtain because of mathematical complications. As a result, choice of estimator in practice has been largely arbitrary. In this paper, we present a systematic study on major target estimators reported in the literature. Focus is on comparisons between the traditional angle method, the line method, and a recently developed line-to-point transformation method. Insights gained from the study directly lead to the development of a novel two-stage angle method that not only produces highly accurate target estimation among all known estimators but is also computationally efficient. © 1998 John Wiley & Sons, Inc. Naval Research Logistics 45: 353–364, 1998 相似文献
998.
This article describes a heuristic and two exact algorithms for several classes of vehicle routing problems defined on tree networks. These include capacitated and time‐constrained vehicle routing problems. One of the exact algorithms is based on the computation of bin packing lower bounds. The other uses column generation. The first algorithm performs better on problems containing small customer demands and in which all vehicles are identical. Otherwise, the second algorithm is more powerful and more versatile. © 1999 John Wiley & Sons, Inc. Naval Research Logistics 46: 75–89, 1999 相似文献
999.
Vic Baston 《海军后勤学研究》1999,46(3):335-340
A new upper bound is obtained for the two‐person symmetric rendezvous value on the real line when the distribution function of their initial distance apart is bounded. A second result shows that if three players are placed randomly on adjacent integers on the real line facing in random directions and able to move at a speed of at most 1, then they can ensure a three‐way meeting time of at most 7/2; the fact that 7/2 is a best possible result follows from work already in the literature. © 1999 John Wiley & Sons, Inc. Naval Research Logistics 46: 335–340, 1999 相似文献
1000.
以经典的机翼/挂架/导弹组合模型为例,采用重叠网格软件系统和计算流体力学技术,从机弹干扰工况简化和气动干扰特性影响因素分析两个方面对外挂式导弹机弹分离气动干扰特性进行研究。导弹分离轨迹参数和气动干扰系数的数值预示结果与捕获轨迹试验结果吻合,表明该计算方法能有效预测机弹分离轨迹和分析导弹与载机间复杂气动干扰现象。根据计算流体力学结果,从马赫数、机翼攻角、导弹攻角等方面,给出导弹在不同分离工况下的气动干扰规律,并采用增量系数法对缺失工况进行一阶外插处理的气动干扰数据外推方法,可应用于机载外挂空基武器的机弹分离轨迹预示和气动干扰特性设计中,具有重要的工程应用价值。 相似文献