基于输出协方差配置的车辆振动控制系统设计

通过对车辆振动系统的振动特性分析,确定出系统反馈控制的设计目标。基于对［１］中状态协方差配置控制理论的推广,文中给出了控制器设计的具体方法,并举例说明该设计方法具有直接有效的特点     

氙原子在铂表面散射的分子动力论方法

运用分子动力论方法研究气体分子 (Xe)在固壁表面 (Pt)的散射。在构造了合理的气体分子与固壁表面相互作用势模型之后 ,运用随机经典轨道方法求解气体分子及固壁原子的运动方程 ,得到气体分子运动轨迹及散射后的运动状态。结果表明 ,气体分子散射后的角度分布与Maxwellian模型存在较大差异 ,而速度基本服从半空间的Maxwellian分布。     

Coherent systems based on sequential order statistics

The sequential order statistics (SOS) are a good way to model the lifetimes of the components in a system when the failure of a component at time t affects the performance of the working components at this age t. In this article, we study properties of the lifetimes of the coherent systems obtained using SOS. Specifically, we obtain a mixture representation based on the signature of the system. This representation is used to obtain stochastic comparisons. To get these comparisons, we obtain some ordering properties for the SOS, which in this context represent the lifetimes of k‐out‐of‐n systems. In particular, we show that they are not necessarily hazard rate ordered. © 2011 Wiley Periodicals, Inc. Naval Research Logistics, 2011     

The minmax multidimensional knapsack problem with application to a chance‐constrained problem

In this paper we present a new combinatorial problem, called minmax multidimensional knapsack problem (MKP), motivated by a military logistics problem. The logistics problem is a two‐period, two‐level, chance‐constrained problem with recourse. We show that the MKP is NP‐hard and develop a practically efficient combinatorial algorithm for solving it. We also show that under some reasonable assumptions regarding the operational setting of the logistics problem, the chance‐constrained optimization problem is decomposable into a series of MKPs that are solved separately. © 2007 Wiley Periodicals, Inc. Naval Research Logistics, 2007     

Parallel machine scheduling with eligibility constraints: A composite dispatching rule to minimize total weighted tardiness

We study a parallel machine scheduling problem, where a job j can only be processed on a specific subset of machines M_j, and the M_j subsets of the n jobs are nested. We develop a two‐phase heuristic for minimizing the total weighted tardiness subject to the machine eligibility constraints. In the first phase, we compute the factors and statistics that characterize a problem instance. In the second phase, we propose a new composite dispatching rule, the Apparent Tardiness Cost with Flexibility considerations (ATCF) rule, which is governed by several scaling parameters of which the values are determined by the factors obtained in the first phase. The ATCF rule is a generalization of the well‐known ATC rule which is very widely used in practice. We further discuss how to improve the dispatching rule using some simple but powerful properties without requiring additional computation time, and the improvement is quite satisfactory. We apply the Sequential Uniform Design Method to design our experiments and conduct an extensive computational study, and we perform tests on the performance of the ATCF rule using a real data set from a large hospital in China. We further compare its performance with that of the classical ATC rule. We also compare the schedules improved by the ATCF rule with what we believe are Near Optimal schedules generated by a general search procedure. The computational results show that especially with a low due date tightness, the ATCF rule performs significantly better than the well‐known ATC rule generating much improved schedules that are close to the Near Optimal schedules. © 2017 Wiley Periodicals, Inc. Naval Research Logistics 64: 249–267, 2017     

带三维落角约束的寻的导弹制导与姿控系统设计

针对带三维落角约束的寻的导弹制导与姿态控制系统设计问题,提出一种基于终端滑模控制和扩张状态观测器的六自由度制导控制系统设计方法。建立包含模型不确定项的寻的导弹六自由度质心与绕质心模型,设计内外双层环路六自由度制导控制系统框架;基于弹-目三维相对运动模型和坐标系转移矩阵建立以攻角和侧滑角为输入的三维全耦合导引方程,利用终端滑模控制方法和扩展状态观测器得到期望的攻角和侧滑角并将其转化为对应的俯仰、偏航和滚转角指令;根据线性形式的寻的导弹绕质心动力学方程,设计与俯仰、偏航和滚转角相关的滑模面向量,并利用终端滑模控制方法和扩张状态观测器得到寻的导弹的副翼偏角、方向舵偏角和俯仰舵偏角指令。六自由度数值仿真结果验证了该方法的有效性和鲁棒性,并证明了该制导控制系统设计方法能以较少的控制设计参数完成预设的制导控制任务。     

平流层飞艇抗风场干扰约束Unscented卡尔曼滤波算法设计与应用

为了提高风场干扰环境下飞艇的导航精度,研究飞艇抗风场干扰导航算法。在建立风场干扰条件下飞艇速度误差约束模型的基础上,设计抗风场干扰的约束Unscented卡尔曼滤波算法。确定风场干扰条件下飞艇的速度误差约束量,将该约束与Unscented卡尔曼滤波算法相结合,对速度误差进行估计和补偿,以减小风场对飞艇定位精度的影响;证明该算法的状态估计量不仅是无偏的,而且协方差小于标准Unscented卡尔曼滤波的协方差;将提出的算法应用于捷联惯导/天文/合成孔径雷达组合导航系统中进行仿真验证,并与自适应扩展卡尔曼滤波和抗差自适应Unscented卡尔曼滤波算法进行比较。结果表明:提出的约束Unscented卡尔曼滤波算法的滤波性能明显优于自适应扩展卡尔曼滤波和抗差自适应Unscented卡尔曼滤波算法,能够有效抑制风场对飞艇定位精度的影响,提高飞艇的导航定位精度。     

北斗卫星伪距信号质量评估及偏差校正

针对北斗卫星信号存在系统性伪距偏差的问题,从多路径角度评估北斗三频信号的质量,验证了该项偏差与卫星轨道类型、卫星仰角及信号频率有关。为消除这一系统性偏差的影响,采用连续分段线性函数建立北斗三频伪距偏差校正模型。与现有的改正模型所不同,所提模型不仅采用了更长时间范围内的北斗实测数据,更为重要的是它顾及了改正数的精度信息。基于动态精密单点定位的实验结果表明,采用所提方法修正后,接收机定位性能有明显提升。     

A sequential scheduling problem with impatient jobs

There are n customers that need to be served. Customer i will only wait in queue for an exponentially distributed time with rate λ_i before departing the system. The service time of customer i has distribution F_i, and on completion of service of customer i a positive reward r_i is earned. There is a single server and the problem is to choose, after each service completion, which currently in queue customer to serve next so as to maximize the expected total return. © 2015 Wiley Periodicals, Inc. Naval Research Logistics 62: 659–663, 2015     

基于GSPN的舰载服务器系统可靠性建模及分析

提出一种基于广义随机Petri网(Generalized Stochastic Petri Net,GSPN)的舰载服务器系统可靠性分析方法。深入分析舰载服务器系统故障模式的基础上,建立冗余服务器子系统的GSPN模型和共享数据盘子系统的GSPN模型,进而综合得到舰载服务器系统的全局GSPN模型,有效模拟了舰载服务器系统的动态行为。仿真实验验证了所提方法的有效性,为舰载服务器系统的分析与设计提供理论参考。