Reliability of linear multistate multiple sliding window systems

This paper proposes a new model that generalizes the linear consecutive k‐out‐of‐r‐from‐n:F system to multistate case with multiple failure criteria. In this model (named linear multistate multiple sliding window system) the system consists of n linearly ordered multistate elements (MEs). Each ME can have different states: from complete failure up to perfect functioning. A performance rate is associated with each state. Several functions are defined for a set of integer numbers ρ in such a way that for each r ∈ ρ corresponding function f_r produces negative values if the combination of performance rates of r consecutive MEs corresponds to the unacceptable state of the system. The system fails if at least one of functions f_r for any r consecutive MEs for r ∈ ρ produces a negative value. An algorithm for system reliability evaluation is suggested which is based on an extended universal moment generating function. Examples of system reliability evaluation are presented. © 2005 Wiley Periodicals, Inc. Naval Research Logistics, 2005.     

A generalized model for estimation of aerodynamic forces and moments for irregularly shaped bodies

A novel method for estimation of an aerodynamic force and moment acting on an irregularly shaped body (such as HE projectile fragments) during its flight through the atmosphere is presented. The model assumes that fragments can be approximated with a tri-axial ellipsoid that has continuous surface given as a mathematical function. The model was validated with CFD data for a tri-axial ellipsoid and verified using CFD data on aerodynamic forces and moments acting on an irregularly shaped fragment.The contribution of this method is that it represents a significant step toward a modeling that does not require a cumbersome CFD simulation results for estimation of fragment dynamic and kinematic parameters. Due to this advantage, the model can predict the fragment motion consuming a negligible time when compared to the corresponding time consumed by CFD simulations. Parametric representation (generalization) of the fragment geometrical data and the conditions provides the way to analyze various correlations and how parameters influence the dynamics of the fragment flight.     

Minimal LST representations of MAP(n)s: Moment fittings and queueing approximations

A Markovian arrival process of order n, MAP(n), is typically described by two n × n transition rate matrices in terms of rate parameters. While it is straightforward and intuitive, the Markovian representation is redundant since the minimal number of parameters is n² for non‐redundant MAP(n). It is well known that the redundancy complicates exact moment fittings. In this article, we present a minimal and unique Laplace‐Stieltjes transform (LST) representations for MAP(n)s. Even though the LST coefficients vector itself is not a minimal representation, we show that the joint LST of stationary intervals can be represented with the minimum number of parameters. We also propose another minimal representation for MAP(3)s based on coefficients of the characteristic polynomial equations of the two transition rate matrices. An exact moment fitting procedure is presented for MAP(3)s based on two proposed minimal representations. We also discuss how MAP(3)/G/1 departure process can be approximated as a MAP(3). A simple tandem queueing network example is presented to show that the MAP(3) performs better than the MAP(2) in queueing approximations especially under moderate traffic intensities. © 2016 Wiley Periodicals, Inc. Naval Research Logistics 63: 549–561, 2016     

离散条件下数字图像矩不变量不变性的分析与研究

对离散条件下数字图像矩不变量的旋转和尺度不变性进行分析,证实了图像识别中采用的矩不变量存在较大变化范围.针对矩不变量变化的主要原因,给出了改进方法,并用实验加以验证.     

Kriging与改进一次二阶矩融合的可靠性分析方法

针对结构可靠性分析问题,提出了Kriging与改进一次二阶矩方法相融合的分析方法。传统的改进一次二阶矩需要计算结构功能函数的梯度信息,在处理包含有限元模型的隐式极限状态问题时会比较困难。该方法将Kriging代理模型与改进一次二阶矩迭代有效而充分地结合,借助Kriging方法提供功能函数的梯度信息,以解决隐式极限状态函数的求导难题,提高分析效率。通过数值与工程算例验证了所提方法的可行性和高效性。     

长码直扩信号的符号速率盲估计方法

针对长码直接序列扩频(DSSS)信号的符号速率估计的难题,提出了基于相关处理的方法。该方法首先估计长码直扩信号的相关函数二阶矩,然后将相关函数二阶矩的估计作为输入信号进行预处理,以去除扩频码周期处的峰值。对预处理后的信号再次进行自相关处理,则所得的信号的频谱中含有符号速率谱线。理论分析和计算机仿真证明了所提出的算法的有效性。     

粘性对高超声速飞行器攻角特性影响研究

采用二维耦合隐式NS方程和标准κ-ε湍流模型对高超声速飞行器在进气道关闭、发动机通流以及发动机点火工作状态下的内外流场进行了数值仿真研究,离散采用二阶迎风格式,分析了在不同攻角(-10°～7°)条件下,粘性对处于三种不同的工作状态下高超声速飞行器升力特性、阻力特性以及俯仰力矩特性的影响.结果表明,粘性对处于发动机通流和发动机点火工作状态下的飞行器气动-推进性能影响显著,尤其是阻力特性,粘性阻力占总阻力的比重超过50%.     

PWM调制方式对六相无刷直流电动机转矩脉动的影响分析

建立了六相无刷直流电动机(BLDC)的相绕组数学模型,在此基础上分析了该电机在 PWM 调制方式下的非换相期间关断相电流的产生过程.分析结果表明,在采用PWM_ON_PWM调制方式时,可以消除多相 BLDC 的非换相期间关断相电流,因此可以降低转矩脉动.此外,还分析了该电机在换相期间的转矩脉动情况,得到了由换相引起的转矩脉动解析表达式,并给出了消除转矩脉动应该满足的 PWM 占空比控制条件.     

六相无刷直流电动机谐波转矩的分析与计算

无刷直流电动机具有诸多优点,但运行中仍然存在转矩脉动问题.分析了六相无刷直流电动机的工作原理,推导了六相无刷直流电动机的状态方程,采用状态变量法对电机转矩产生的关键量--反电势波形和电流波形进行了仿真和试验研究,对六相无刷直流电动机的谐波转矩进行了分析和推导,得出了通过减小电流滞后角可控制甚至消除正弦谐波脉动转矩的结论.     

失效概率函数求解的高效算法

结合基于分数矩约束的极大熵方法和替代模型法,发展了一种失效概率函数求解的高效算法。所提算法的基本思路是利用自主学习的迭代Kriging方法来构造失效概率函数,即采用较少的训练样本来构造粗糙的失效概率函数,在此基础上通过添加新的违反学习函数约束的样本来更新失效概率函数,直到达到精度要求。对于每一个分布参数的训练样本点,所提方法采用分数矩约束的极大熵法来求解相应的失效概率样本。由于分数矩的计算采用了高效的降维积分,并且由于分数矩约束下极大熵法中优化策略高效地逼近了响应的概率密度函数,从而使得失效概率样本能够被高效高精度地估计出来。为了检验所提方法的精度及效率,给出了两个算例,对比了所提方法与已有的失效概率函数求解的Bayes公式法及Monte Carlo法等,结果表明,所提方法适用于求解复杂的功能函数问题,且在满足精度要求的基础上大大降低了计算量。