双机空战的仿真与分析

用矩阵博弈理论、计算机仿真的方法研究了空战过程,使双机的空中格斗阶段─目标的跟踪、射击、弹道计算及射击效果的评定连续化,并用ＦＯＲＴＲＡＮ─７７语言编程在计算机上进行了Ｆ＿Ａ、Ｆ＿Ｂ两种飞行的空战,仿真结果与实际情况基本一致。本程序具有通用性,可对不同种类的飞机及武器系统的性能作出定性和定量的分析和评估。     

C~3l系统软件质量保障技术研究

针对C~3I 软件系统设计实现中所存在的问题,文章重点对软件质量保障方法进行了分析研究,同时提出一种简化任务评审阶段的软件质量综合保障建议。对从事C~3I 系统工程软件质量保障的人员可供参考。     

系统状态方程的信流图描述

本文从基本概念出发,结合两个具体电路讨论如何用信流图建立系统标准状态方程的方法。     

微波雷达目标信号模拟器及其应用

本文为在野战条件下检测雷达测距系统的性能提供一种新型微波目标信号模拟器,闸述其工作原理及功能。除在检测雷达测距系统性能上已得到实际应用外,还论述了可以进一步开发的应用项目,因为不受场地和气候条件的限制,从而获得较好的效能、效率和效益。     

A nonparametric Bayes approach to decide system burn-in time

Burn-in is the preconditioning of assemblies and the accelerated power-on tests performed on equipment subject to temperature, vibration, voltage, radiation, load, corrosion, and humidity. Burn-in techniques are widely applied to integrated circuits (IC) to enhance the component and system reliability. However, reliability prediction by burn-in at the component level, such as the one using the military (e.g., MIL-STD-280A, 756B, 217E [23–25]) and the industrial standards (e.g., the JEDEC standards), is usually not consistent with the field observations. Here, we propose system burn-in, which can remove many of the residual defects left from component and subsystem burn-in (Chien and Kuo [6]). A nonparametric model is considered because 1) the system configuration is usually very complicated, 2) the components in the system have different failure mechanisms, and 3) there is no good model for modeling incompatibility among components and subsystems (Chien and Kuo [5]; Kuo [16]). Since the cost of testing a system is high and, thus, only small samples are available, a Bayesian nonparametric approach is proposed to determine the system burn-in time. A case study using the proposed approach on MCM ASIC's shows that our model can be applied in the cases where 1) the tests and the samples are expensive, and 2) the records of previous generation of the products can provide information on the failure rate of the system under investigation. © 1997 John Wiley & Sons, Inc. Naval Research Logistics 44: 655–671, 1997     

Solution algorithms for the parallel replacement problem under economy of scale

We consider the parallel replacement problem in which machine investment costs exhibit economy of scale which is modeled through associating both fixed and variable costs with machine investment costs. Both finite- and infinite-horizon cases are investigated. Under the three assumptions made in the literature on the problem parameters, we show that the finite-horizon problem with time-varying parameters is equivalent to a shortest path problem and hence can be solved very efficiently, and give a very simple and fast algorithm for the infinite-horizon problem with time-invariant parameters. For the general finite-horizon problem without any assumption on the problem parameters, we formulate it as a zero-one integer program and propose an algorithm for solving it exactly based on Benders' decomposition. Computational results show that this solution algorithm is efficient, i.e., it is capable of solving large scale problems within a reasonable cpu time, and robust, i.e., the number of iterations needed to solve a problem does not increase quickly with the problem size. © 1998 John Wiley & Sons, Inc. Naval Research Logistics 45: 279–295, 1998     

Single machine sequencing with linear models of release dates

The paper deals with a problem of scheduling a set of jobs on a single machine. Before a job is released for processing, it must undergo some preprocessing treatment that consumes resources. It is assumed that the release date of a job is a linear decreasing continuous function of the amount of a locally and globally constrained, continuously divisible resource (e.g., energy, catalyzer, financial outlay, gas). The problem is to find a sequence of jobs and a resource allocation that will minimize the maximum job completion time. Such a problem appears, for example, in the ingot preheating and hot-rolling process in steel mills. It is shown that the problem is strongly NP-hard. Some polynomially solvable cases of the problem and approximate algorithms with both experimental and worst-case analysis are presented. © 1998 John Wiley & Sons, Inc. Naval Research Logistics 45: 99–113, 1998     

Attrition models of the Ardennes campaign

This paper revisits the modeling by Bracken [3] of the Ardennes campaign of World War II using the Lanchester equations. It revises and extends that analysis in a number of ways: (1) It more accurately fits the model parameters using linear regression; (2) it considers the data from the entire campaign; and (3) it adds in air sortie data. In contrast to previous results, it concludes by showing that neither the Lanchester linear or Lanchester square laws fit the data. A new form of the Lanchester equations emerges with a physical interpretation. © 1998 John Wiley & Sons, Inc. Naval Research Logistics 45: 1–22, 1998     

扩张状态观测器的观测误差前馈补偿设计

在"总和"扰动模型未知的前提下,针对线性扩张状态观测器跟踪时变信号精度不高的问题,设计出一种前馈观测补偿器。在分析线性扩张状态观测器观测原理的基础上,通过对扰动项的线性近似、误差系统动态响应的忽略,在时域内推导出观测静差的量化表达式,进而使用扰动微分项的估计值替代真值对观测作前馈补偿。理论分析了替代的可行性,证明了补偿器减小观测误差幅值、超前校正观测相位滞后的作用。将这一补偿思想推广至非线性扩张状态观测器中。通过仿真对补偿器提高观测精度、加快误差收敛的有效性进行检验,实验结果进一步表明,补偿器的引入能显著提高整个自抗扰控制系统的控制精度,从而证明了这种补偿思路的可行性。     

针对不同视场辅助信标的无人机目标定位方法

针对无人机在单站测角测距的目标定位过程中受无人机姿态角误差影响较大的问题,提出一种对辅助信标进行探测并与惯性传感器相结合的无人机姿态求解方法。建立基于容积卡尔曼滤波的惯性传感器姿态求解模型,采用梯度下降法对基于辅助信标的无人机位姿参数进行求解,并综合它们的结果对无人机的姿态偏差进行估计和校正,最后完成了不同视场条件下的目标定位和仿真计算。结果表明,所提方法对无人机目标定位精度有明显提高。