The Early Responses of Air-backed plate subjected to underwater explosion with aluminized explosives

This work aims to research the effects on the early responses of the air-backed plate subjected to the loading generated by the underwater explosion with aluminized explosives. The loading characteristics of underwater explosion for ideal explosive (TNT), aluminized explosives (RS211 and RBUL) are obtained experimentally. The tested aluminized explosives have different energy output compared with TNT. Based on the Taylor plate theory, the early responses of the air-backed steel plate affected by the measured loading is analyzed. The analytical results indicate that the pressure curve of the shock wave within 1 time decay constant is the main factor affecting the kick-off velocity of the plate when cavitation occurring. The velocity responses of the plate produced by the loading of RS211 and RBUL are obviously different with that of an equivalent TNT charge, which also indicates validity and suitability should be noticed in the case of substituting TNT for aluminized explosives. Moreover, the uncertainties in the responses of the plate produced by RS211 and RBUL are much larger than TNT.     

On competitive analysis for polling systems

Polling systems have been widely studied, however most of these studies focus on polling systems with renewal processes for arrivals and random variables for service times. There is a need driven by practical applications to study polling systems with arbitrary arrivals (not restricted to time-varying or in batches) and revealed service time upon a job's arrival. To address that need, our work considers a polling system with generic setting and for the first time provides the worst-case analysis for online scheduling policies in this system. We provide conditions for the existence of constant competitive ratios, and competitive lower bounds for general scheduling policies in polling systems. Our work also bridges the queueing and scheduling communities by proving the competitive ratios for several well-studied policies in the queueing literature, such as cyclic policies with exhaustive, gated or l-limited service disciplines for polling systems.     

Exact analysis of (R,s, S) inventory control systems with lost sales and zero lead time

We study an (R, s, S) inventory control policy with stochastic demand, lost sales, zero lead‐time and a target service level to be satisfied. The system is modeled as a discrete time Markov chain for which we present a novel approach to derive exact closed‐form solutions for the limiting distribution of the on‐hand inventory level at the end of a review period, given the reorder level (s) and order‐up‐to level (S). We then establish a relationship between the limiting distributions for adjacent values of the reorder point that is used in an efficient recursive algorithm to determine the optimal parameter values of the (R, s, S) replenishment policy. The algorithm is easy to implement and entails less effort than solving the steady‐state equations for the corresponding Markov model. Point‐of‐use hospital inventory systems share the essential characteristics of the inventory system we model, and a case study using real data from such a system shows that with our approach, optimal policies with significant savings in inventory management effort are easily obtained for a large family of items.     

灵活的多层嵌套拉丁超立方体设计构造

计算机试验的设计方法越来越受到重视,嵌套拉丁超立方体设计是计算机试验设计中的一种新型方法,其在多种精度试验中有广泛的应用。但多数嵌套拉丁超立方体设计要求低精度试验次数需为高精度试验次数的倍数,这在应用中会有很大的局限性。通过对其构造方法的改进,得到一种结构更加灵活的多层嵌套拉丁超立方体设计,使得不同精度试验的次数可以更加灵活选取。该设计方法在一维投影上可以达到很好的均匀性。仿真结果表明,该方法较若干相关方法能够达到更小的均方误差。     

基于先验信息的分布式星载单基线SAR/ATI方法

在综述了分布式星载SAP/ATI技术的基础上,阐述了单基线SAP/ATI技术的原理和杂波、噪声对检测、测速性能的影响,给出了一种基于先验信息的单基线SAR/ATI检测和测速方法,最后基于多功能的天基雷达仿真系统进行了仿真实验和性能分析.     

模拟油罐油气混合物爆炸实验与数值仿真研究

对模拟油罐内油气混合物爆炸冲击波特性进行了研究.在直径为1 m的模拟油罐中进行了油气混合物爆炸模拟实验,建立了模拟油罐油气混合物爆炸的数值仿真模型,并借助大型商业软件Fluent6.2完成了数值仿真研究.数值仿真结果与实验值较为吻合.模拟实验和数值仿真研究的结果表明:油气体积分数、罐内初始温度等决定模拟油罐油气混合物爆炸压力的大小.油罐内爆炸压力波的振荡特性对金属油罐结构来说是有害的.     

基于IMM-RUASFF的网络化目标跟踪算法

针对目前网络化目标跟踪算法存在实时性差、精度低等问题进行了研究。首先,基于网络信息共享需求,建立了网络探测节点的目标跟踪模型;其次,网络探测节点目标跟踪需求和实战要求发现目标经常是有多种运动状态并存,而单一模型的滤波器不能满足对机动目标跟踪性能的要求,采用了基于交互式多模型(Interacting Multiple Model,IMM)的有反馈实时更新的异步状态融合算法。最后,针对多个探测节点目标跟踪的状态融合估计问题,提出了一种有反馈实时更新的异步状态融合算法,通过仿真验证了算法的有效性。     

多约束下的高超声速飞行器三维非线性自适应末制导律

面向多约束下高超声速飞行器末制导过程中的通道耦合、参数扰动、模型失配等突出问题,设计一种适于高超声速飞行器的三维非线性自适应末制导律。为了模型描述的完整性和简洁性,引入视线旋量和旋量速度的概念,并基于此建立三维制导参考模型和实际系统的表达式;为了保证制导律的鲁棒性和自适应性,基于自适应控制理论,设计一种三维非线性自适应制导律;通过数学推导证明了该制导律的稳定性。该制导律能够从理论上克服高超声速飞行器末制导面临的通道耦合、参数扰动、模型失配等突出问题,满足多约束制导要求。仿真结果验证了所设计制导律的有效性。     

含轴间距误差的消隙齿轮刚柔耦合动力学仿真

轴间距误差对消隙齿轮精度和性能有重要影响,但其机理和规律并不清楚。基于接触碰撞力约束关系建立齿轮接触动力学模型,进一步利用ADAMS/Flex建立单级消隙齿轮传动系统的刚柔耦合模型,通过刚柔耦合动力学仿真研究消隙齿轮传动在不同轴间距制造误差条件下的振动及频率特性。研究发现:随着轴间距的减小,扭簧的平均力矩增大,齿轮齿面间的啮合力矩以及摩擦力矩也将增大,从而阻碍扭矩的正常传递,并导致固定齿轮转速幅值降低;随着轴间距的增大,固定齿轮主谐振频率整体上降低,而且在轴间距稍大于标准中心距时降低很快。这一发现可指导消隙齿轮传动的设计和装配。     

应用边界交叉法的高超声速滑翔飞行器多目标轨迹优化

针对高超声速滑翔飞行器复杂约束条件下多目标轨迹设计问题,基于边界交叉法和伪谱法提出多目标轨迹优化方法。分析高超声速滑翔飞行器复杂约束轨迹优化问题的特点,提出多目标轨迹优化问题。采用边界交叉法和伪谱法将多目标轨迹优化问题转化为一组单目标优化子问题,利用非线性规划算法分别求解。在优化过程中,将已求解子问题的解作为下一个子问题的初始值,求解最大横程和最小峰值热流轨迹优化问题。仿真结果表明:所提方法能够有效搜索到优化轨迹的Pareto前沿,可以为高超声速滑翔飞行器轨迹设计提供参考。