创新人才军民融合培养体系及其构建

创新人才军民融合培养构成人才强国战略、创新驱动发展战略和军民融合发展战略的交汇点。创新人才是战略资源,军民融合为创新人才培养提供了一条全新路径。作为一项系统工程,创新人才军民融合培养包括创新人才军民融合培养主体系统、创新人才军民融合培养客体系统、创新人才军民融合培养方案系统、创新人才军民融合培养资源系统、创新人才军民融合培养制度系统、创新人才军民融合培养考评系统,在系统构建过程中需加大统筹协调、投入保障、政策倾斜、法治保障、合理使用力度,注重体系推进。     

Dynamic server assignment policies for assembly‐type queues with flexible servers

We seek dynamic server assignment policies in finite‐capacity queueing systems with flexible and collaborative servers, which involve an assembly and/or a disassembly operation. The objective is to maximize the steady‐state throughput. We completely characterize the optimal policy for a Markovian system with two servers, two feeder stations, and instantaneous assembly and disassembly operations. This optimal policy allocates one server per station unless one of the stations is blocked, in which case both servers work at the unblocked station. For Markovian systems with three stations and instantaneous assembly and/or disassembly operations, we consider similar policies that move a server away from his/her “primary” station only when that station is blocked or starving. We determine the optimal assignment of each server whose primary station is blocked or starving in systems with three stations and zero buffers, by formulating the problem as a Markov decision process. Using this optimal assignment, we develop heuristic policies for systems with three or more stations and positive buffers, and show by means of a numerical study that these policies provide near‐optimal throughput. Furthermore, our numerical study shows that these policies developed for assembly‐type systems also work well in tandem systems. © 2008 Wiley Periodicals, Inc. Naval Research Logistics, 2008     

基于χ~2检验的惯性/卫星紧耦合系统故障检测与隔离方法

研究了一种基于χ~2检验的惯性/卫星紧耦合系统故障检测与隔离方法,该方法可利用故障检测函数自动识别单个卫导故障,并实时剔除故障星重构观测信息序列,从而避免了对紧耦合系统的影响。构建数字化仿真环境对所研究的故障检测与隔离方法进行了仿真,仿真结果表明,该方法可在卫星发生故障时及时检测并隔离故障星,并自动实现观测信息重构,保证了紧耦合系统的精度和完好性。     

地面站对月球探测器的导航

针对一个从地球停泊轨道出发绕地月飞行的月球探测器 ,讨论地面站对月球探测器导航的几个问题 ,包括观测方式的选取、地面站的分布、制导点的调整、导航精度等。结果表明仅依靠局域的地面站 ,采用测距的方式 ,可以对探测器进行实时导航。研究的方法和结果可供月球探测实际工程参考     

一种捷联惯导系统姿态测量新算法的应用研究

为改进捷联惯导系统姿态矩阵的解算、实时计算等问题,本文引入四元数三阶泰勒展开递推式作为捷联惯导系统的姿态更新算法,着重解决了使用三阶泰勒展开递推式进行姿态计算的方法,并对某陆地捷联惯导系统的量测数据,用C语言进行了相应的仿真.本文的工作为改进捷联惯导系统算法提供了参考依据.     

地炮营通信系统载波监听／碰撞检测仿真分析

给出某地炮营通信系统信息传输的CSMA／CD(Carrier Sense Multiple Acces／Collision Detection)排队论模型,提出了信道争用和碰撞的问题,用单机和网络仿真分析了载波监听条件下通信失效的概率,给出信道争用和碰撞的几个性能指标,并利用软件的方法,提供了减少碰撞的方案     

信息战战场分析模型

根据区域攻防的不同战场信息行动,建立3个非线性微分方程模型.以防御方的总射击速率和战斗力消耗率作为评价指标,着重探讨了进攻方的指挥控制系统、侦察监视系统、战毁评估系统和火力系统之间的性能匹配关系.     

GPS仿真器设计

本文详细介绍了在无人机利用ＧＰＳ导航半实物仿真系统中ＧＰＳ仿真器的设计原理。通过分析ＧＰＳ及ＧＰＳ接收机的基本工作方式,ＷＧＳ－８４与各种坐标系的转换关系,研制了ＧＰＳ仿真器。它将由飞行仿真计算机得到的无人机位置信息转换成与之对应的ＧＰＳ信号,输入飞控计算机,以实现ＧＰＳ导航的仿真试验。     

具有规范化的四元数递推计算的公式误差估计

对捷联式制导系统中目前常用的四元数递推公式进行误差估计,给出利用观测数据计算四元数的误差界的公式,还介绍了保持四元数范数不变的一类递推公式。     

Performance analysis of queue length monitoring of M/G/1 systems

This study investigates the statistical process control application for monitoring queue length data in M/G/1 systems. Specifically, we studied the average run length (ARL) characteristics of two different control charts for detecting changes in system utilization. First, the nL chart monitors the sums of successive queue length samples by subgrouping individual observations with sample size n. Next is the individual chart with a warning zone whose control scheme is specified by two pairs of parameters, (upper control limit, d_u) and (lower control limit, d_l), as proposed by Bhat and Rao (Oper Res 20 (1972) 955–966). We will present approaches to calculate ARL for the two types of control charts using the Markov chain formulation and also investigate the effects of parameters of the control charts to provide useful design guidelines for better performance. Extensive numerical results are included for illustration. © 2011 Wiley Periodicals, Inc. Naval Research Logistics, 2011