姿控发动机脉冲工作的管路瞬变特性

采用有限差分格式的特征线方法 ,对某姿控推进系统发动机真实推进剂管路在脉冲工作情况下的瞬变特性进行了数值研究 ,对影响发动机多次脉冲启动的重要参数进行了定量计算 ,对比分析了试验结果与计算结果的一致性。说明该方法可方便地对包括许多管路、阀门和推力室的复杂系统进行动态性能分析 ,所得结果对于液体火箭发动机管路工程设计具有重要参考价值     

带紧扰动的m-增生算子的满值性定理

引入“DC”空间的概念,研究了带紧扰动的m－增生算子的满值性问题,改进了Kartsatos、Deimling、周海云以及徐宗本等人的结果。     

Polynomial‐time approximation scheme for concurrent open shop scheduling with a fixed number of machines to minimize the total weighted completion time

In this article, we consider the concurrent open shop scheduling problem to minimize the total weighted completion time. When the number of machines is arbitrary, the problem has been shown to be inapproximable within a factor of 4/3 ‐ ε for any ε > 0 if the unique games conjecture is true in the literature. We propose a polynomial time approximation scheme for the problem under the restriction that the number of machines is fixed. © 2011 Wiley Periodicals, Inc. Naval Research Logistics, 2011     

基因表达缺失值的加权回归估计算法

在基因芯片实验中,数据缺失客观存在,并在一定程度上影响芯片数据后续分析结果的准确性。在不增加实验次数的情况下,缺失值估计是降低缺失数据对后续分析影响的有效方法。利用相似性信息的核加权函数来实现缺失值回归估计的局部化,提出了基于加权回归估计的基因表达缺失值估计算法。在两个不同类型的基因芯片数据上,将新方法与几种已知的方法进行了比较分析。实验结果表明,新的估计算法具有比传统缺失值估计算法更好的稳定性和估计准确度。     

对辐射源信号到达角的自适应跟踪估计

为提高信号到达角(AOA)的测量精度,采用修正的窗函数加权平均算法和基于机动加速度的非零均值时间相关模型的自适应卡尔曼滤波算法,将信号到达角的变化轨迹看作是一种做加速度机动的运动,实现对连续变化信号到达角的参数估计.计算机仿真验证了算法的有效性和可行性,证明该方法有一定的应用价值.     

多输出性能下的重要性测度指标及其求解方法

针对基于马氏距离的重要性测度存在的问题,提出了基于谱分解加权摩尔彭罗斯马氏距离的重要性测度指标,通过构造多输出协方差阵的广义逆矩阵以及谱分解的策略,有效解决了协方差阵求逆奇异情况以及由于未能充分考虑多输出之间的相互关系而导致的错误识别重要变量的问题,克服了基于马氏距离指标的局限性。数值算例与工程算例结果表明:所提重要性测度可以更加准确地获得输入变量对结构系统多输出性能随机取值特征贡献的排序,从而为可靠性设计提供充分的信息。     

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     

基于非线性Kalman滤波的导航系统误差补偿技术

针对非线性非高斯导航系统信息处理问题,采用自组织算法、神经网络和遗传算法等改进传统非线性Kalman滤波算法,构建一种自适应的组合导航系统。应用具有冗余趋势项的自组织算法、Volterra神经网络和遗传算法,建立导航系统误差的非线性预测模型,进而计算得到其预测值;将该预测值与Kalman滤波算法求得的估计值进行比较得到差值,以此监测Kalman滤波算法的工作状态;采用自适应控制方法,在导航系统结构层面改进Kalman滤波算法,构建新型的导航系统误差补偿模型。开展基于导航系统KIND-34的半实物仿真研究,应用所提出的改进方法改善了导航系统误差的补偿效果,提高了组合导航系统的自适应能力和容错能力。     

非线性支撑下悬臂输流管道的Hopf分叉特性

研究了外激励作用下非线性支撑悬臂输流管道系统的Hopf分叉特性,建立了外激励作用下非线性支撑悬臂输流管道系统的动力学方程,并采用Galerkin方法离散动力学方程,由增量谐波平衡(IHB)法推导了方程的近似解析解,由Floquet理论判定了解的稳定性,同时给出了系统的Hopf分叉点。利用数值算法和IHB法研究了支撑位置、支撑结构刚度和阻尼对系统Hopf分叉特性的影响规律。研究表明:系统的幅频特性在Hopf分叉前后发生了改变,响应频率由外激励频率变为系统的自激振动频率,且系统Hopf分叉后,幅值显著增大。该研究结果可为悬臂管道的振动控制提供理论基础。     

两栖型指控车非线性横摇安全盆侵蚀研究

采用单自由度系统研究了两栖型指控车在规则波激励下的非线性横摇和倾覆,非线性横摇控制方程应用四阶龙格库塔法进行数值积分;以波浪扰动力矩的幅值和波浪的频率作为变量,研究了两栖型指控车的安全盆侵蚀问题。以波浪扰动力矩的幅值为变量的安全盆侵蚀研究结果表明:当波浪扰动力矩大于0.01时,安全盆开始出现侵蚀现象,当波浪扰动力矩大于1.84时,安全盆的安全域已经变成了几个离散的点,随着波浪扰动力矩继续增大,安全盆的安全域将继续严重侵蚀,直到消失为止。以波浪频率为变量的安全盆侵蚀研究结果表明:两栖型指控车的安全盆侵蚀对波浪的频率敏感,安全盆出现明显的侵蚀;随着频率的增大,安全盆侵蚀将不会发生,表明两栖型指控车对高频波浪是安全的。