海军诸兵种综合战术训练仿真系统构建研究

如何构建诸军兵种综合战术训练仿真系统,是当前全军训练仿真领域内的研究热点。基于HLA技术框架及分层式RTI,搭建了海军诸兵种综合战术训练仿真系统的体系结构。并采用面向对象的建模与仿真方法,提出了系统公共参考FOM模型的设计思路,定义了实体类、交互类及路径空间,有效规范并减少了系统间网络传输的数据流量。最后,给出了系统仿真实现的流程图和一个仿真实例。实践证明,使用HLA仿真框架实现的海军诸兵种综合战术训练仿真系统能够满足当前海军战术训练的需求。     

机场目标打击顺序灰色决策分析

对军事机场目标的结构、特征进行了系统分析,确立了军事机场目标评估体系,并运用灰色决策分析方法建立了军事机场多目标打击顺序确定的优化模型,为对该类实施导弹打击所进行的火力计划拟制提供了一种新的数学方法。     

Signature based analysis of m‐Consecutive‐k‐out‐of‐n: F systems with exchangeable components

In this article, we study reliability properties of m‐consecutive‐k‐out‐of‐n: F systems with exchangeable components. We deduce exact formulae and recurrence relations for the signature of the system. Closed form expressions for the survival function and the lifetime distribution as a mixture of the distribution of order statistics are established as well. These representations facilitate the computation of several reliability characteristics of the system for a given exchangeable joint distribution or survival function. Finally, we provide signature‐based stochastic ordering results for the system's lifetime and investigate the IFR preservation property under the formulation of m‐consecutive‐k‐out‐of‐n: F systems. © 2011 Wiley Periodicals, Inc. Naval Research Logistics, 2011     

基于HLA的C^4ISRK作战运用仿真系统探讨

C4ISRK是实现未来信息化战场"网络中心战"概念的一组必要的装备系统.着眼于为C4ISRK系统作战运用项目先期概念技术演示提供仿真平台,提出了C4ISRK系统的概念模型,在此基础上重点研究了基于HLA的C4ISRK作战运用仿真系统的总体框架及其设计,为该仿真系统的建立和仿真实施提供了技术支持.     

Failure profiles of coherent systems

In this paper we first introduce and study the notion of failure profiles which is based on the concepts of paths and cuts in system reliability. The relationship of failure profiles to two notions of component importance is highlighted, and an expression for the density function of the lifetime of a coherent system, with independent and not necessarily identical component lifetimes, is derived. We then demonstrate the way that failure profiles can be used to establish likelihood ratio orderings of lifetimes of two systems. Finally we use failure profiles to obtain bounds, in the likelihood ratio sense, on the lifetimes of coherent systems with independent and not necessarily identical component lifetimes. The bounds are relatively easy to compute and use. © 2004 Wiley Periodicals, Inc. Naval Research Logistics, 2004     

Scheduling recurrent construction

A problem we call recurrent construction involves manufacturing large, complex, expensive products such as airplanes, houses, and ships. Customers order configurations of these products well in advance of due dates for delivery. Early delivery may not be permitted. How should the manufacturer determine when to purchase and release materials before fabrication, assembly, and delivery? Major material expenses, significant penalties for deliveries beyond due dates, and long product makespans in recurrent construction motivate choosing a release timetable that maximizes the net present value of cash flows. Our heuristic first projects an initial schedule that dispatches worker teams to tasks for the backlogged products, and then solves a series of maximal closure problems to find material release times that maximize NPV. This method compares favorably with other well‐known work release heuristics in solution quality for large problems over a wide range of operating conditions, including order strength, cost structure, utilization level, batch policy, and uncertainty level. Computation times exhibit near linear growth in problem size. © 2004 Wiley Periodicals, Inc. Naval Research Logistics, 2004     

一种能考虑动升力影响的高速艇迎浪纵向运动的数学模型

根据高速艇在静水及波浪中运动的特点,提出了高速艇迎浪纵向运动的基本假设,建立了能考虑动升力影响的高速艇迎浪纵向运动基本方程,并提出了高速艇迎浪纵向运动预报的一种新方法(滑航法),编制了理论预报程序,进行了模型试验验证研究.结果表明,中高航速时,滑航法可用于高速艇迎浪纵向运动的预报.     

关于值分布论中一个著名猜测的推广

运用Nevanlinna的亚纯函数理论方法,研究了超越亚纯函数的值分布理论,获得了如下的结论:设f为超越亚纯函数,c为f的不恒等于0的的小函数,则当n≥3时,fnf′-c有无穷多个零点;若附加条件f只有有限多个级≤2的零点,则对一切正整数n,fnf′-c都有无穷多个零点.因而对Chiang Y M的问题作出了部分回答.     

适用于公共安全领域的多功能警用无人旋翼机

与直升机和固定翼相比,无人旋翼机对起飞场地的要求较低,具有低能耗、高功效、不易受环境因素影响等优点,适合安保部队的任务需要。为了进一步提高其作战性能,以无人自转旋翼机为平台,添加多种操作功能,完成宣传威慑、高空监控、杀伤性与非杀伤性攻击等任务,进而实现无人自转旋翼机的多功能化。     

航天器交会中的多圈Lambert问题研究

针对大椭圆轨道追踪器固定时间直接碰撞交会问题,介绍了一种快速确定多圈Lambert问题最优解的新方法。研究了多圈Lambert转移解,分析了转移时间与转移轨道参数的关系;研究了无时间约束最优直接碰撞交会及其必要条件。仿真表明:最优解快速确定方法有效、可行,并可提高计算效率。