多操纵面战斗机飞行控制系统设计

现代多操纵面战斗机飞行控制系统多采用非线性控制方法进行设计,其中逆系统方法具有物理概念清晰、参数对应明确、无不确定性算法、容易结合传统经验等优点,易于工程实现.将该方法应用于多操纵面战斗机的基本控制律设计,使用多层简化设计,改进了多操纵面的控制分配策略,并针对某型多操纵面战斗机六自由度模型进行数字仿真,效果良好.     

多核异构冗余模型设计与可靠性分析

为进行电磁仿生研究,提高复杂电磁环境下控制系统运行的可靠性,在一种新型计算机系统结构框架的基础上,提出了多核异构冗余模型,设计了互关总线协议,实现了相应的容错策略,进而进行了异构双机冗余系统的实验,并利用马尔可夫过程模型分析了系统的电磁抗扰能力。实验表明,该模型能够有效地提高系统可靠性,满足相关仿生研究的设计要求。     

On a Markov‐modulated shock and wear process

We present transient and asymptotic reliability indices for a single‐unit system that is subject to Markov‐modulated shocks and wear. The transient results are derived from the (transform) solution of an integro‐differential equation describing the joint distribution of the cumulative degradation process and the state of the modulating process. Additionally, we prove the asymptotic normality of a properly centered and time‐scaled version of the cumulative degradation at time t. This asymptotic result leads to a simple normal approximation for a properly centered and space‐scaled version of the systes lifetime distribution. Two numerical examples illustrate the quality of the normal approximation. © 2009 Wiley Periodicals, Inc. Naval Research Logistics 2009     

鱼雷联接结构可靠性稳健优化设计

将可靠性优化设计理论与可靠性灵敏度分析方法相结合,提出了可靠性稳健优化设计方法.采用该方法对鱼雷螺钉联接结构和楔环联接结构进行了实例分析,并给出了仿真计算结果,为工程实际机械产品的可靠性稳健优化设计提供了理论依据.     

基于预计和评估结果融合的电子装备可靠性预测方法

分析了目前获得电子装备可靠性水平的可靠性预计和评估两种方法各自的优缺点,确立了融合两种方法所得结果以解决各自方法不足的思想.基于证据决策理论,以电子装备累积故障概率作为目标集,将可靠性预计结果和评估结果分别作为两批证据对目标集进行支持.利用信息融合方法,对两个利用不同源信息得出的预计结果和评估结果进行了融合,并得到了准确、实用的可靠性预测结果.最后以某型雷达为例进行实例分析,验证此方法的可行性.     

Bi‐objective missile rescheduling for a naval task group with dynamic disruptions

This paper considers the rescheduling of surface‐to‐air missiles (SAMs) for a naval task group (TG), where a set of SAMs have already been scheduled to intercept a set of anti‐ship missiles (ASMs). In missile defense, the initial engagement schedule is developed according to the initial state of the defensive and attacking units. However, unforeseen events may arise during the engagement, creating a dynamic environment to be handled, and making the initial schedule infeasible or inefficient. In this study, the initial engagement schedule of a TG is assumed to be disrupted by the occurrence of a destroyed ASM, the breakdown of a SAM system, or an incoming new target ASM. To produce an updated schedule, a new biobjective mathematical model is formulated that maximizes the no‐leaker probability value for the TG and minimizes the total deviation from the initial schedule. With the problem shown to be NP‐hard, some special cases are presented that can be solved in polynomial time. We solve small size problems by the augmented ? ‐ constraint method and propose heuristic procedures to generate a set of nondominated solutions for larger problems. The results are presented for different size problems and the total effectiveness of the model is evaluated.     

不同故障模式下的可靠性优化问题

以阀门流体系统为例 ,通过理论分析与数值计算 ,讨论了组成单元具有多个故障模式情形的系统可靠性优化问题 ,对传统的冗余技术作了进一步的发展 ,确立了考虑不同故障模式时可靠性优化的一般模型 ,最后得到了必须根据不同故障模式比率确定配置方式的结论     

可靠性强化试验及其在某型机载吊舱关键模块的应用

针对某型机载吊舱故障频发,可靠性低以及传统可靠性试验周期长、费用高的问题,采用了可靠性强化试验对某型机载吊舱关键模块进行试验研究。阐述了可靠性强化试验的技术、方法和试验过程,给出了强化试验的应力剖面和试验结果。通过强化试验,迅速激发了产品的潜在故障,通过对测试结果初步分析得出了故障原因,为后续改进提供依据,提高了产品的可靠性,并且缩短了试验时间,减少了试验费用,验证了可靠性强化试验的有效性。     

J-M模型改进与可靠性预测研究

软件可靠性J-M预计模型对可靠性测试数据的假设要求比较严格,与实际情况不太符合。针对可靠性测试中各种因素的影响,适当修改了排除错误的条件假设,使得模型的适用性更强。对J-M模型用迭代法确定了参数的估计值,结合1组可靠性测试数据,得到可靠性预测结果。