基于χ~2检验的惯性/卫星紧耦合系统故障检测与隔离方法

研究了一种基于χ~2检验的惯性/卫星紧耦合系统故障检测与隔离方法,该方法可利用故障检测函数自动识别单个卫导故障,并实时剔除故障星重构观测信息序列,从而避免了对紧耦合系统的影响。构建数字化仿真环境对所研究的故障检测与隔离方法进行了仿真,仿真结果表明,该方法可在卫星发生故障时及时检测并隔离故障星,并自动实现观测信息重构,保证了紧耦合系统的精度和完好性。     

小口径舰炮武器系统作战效能评估模型研究

通过对小口径舰炮武器系统的分析,建立小口径舰炮武器系统作战效能评估指标体系,得到基于"串/并联"模型框架的作战效能评估A.D.C扩展模型E=A.D.C.S.通过某型小口径舰炮武器系统的实例计算验证了模型的正确性,并得出分析结论.     

Model parameter estimation and residual life prediction for a partially observable failing system

We consider a partially observable degrading system subject to condition monitoring and random failure. The system's condition is categorized into one of three states: a healthy state, a warning state, and a failure state. Only the failure state is observable. While the system is operational, vector data that is stochastically related to the system state is obtained through condition monitoring at regular sampling epochs. The state process evolution follows a hidden semi‐Markov model (HSMM) and Erlang distribution is used for modeling the system's sojourn time in each of its operational states. The Expectation‐maximization (EM) algorithm is applied to estimate the state and observation parameters of the HSMM. Explicit formulas for several important quantities for the system residual life estimation such as the conditional reliability function and the mean residual life are derived in terms of the posterior probability that the system is in the warning state. Numerical examples are presented to demonstrate the applicability of the estimation procedure and failure prediction method. A comparison results with hidden Markov modeling are provided to illustrate the effectiveness of the proposed model. © 2015 Wiley Periodicals, Inc. Naval Research Logistics 62: 190–205, 2015     

高分辨率UAV SAR的三维运动误差分离与补偿

在基于SAR回波的数据处理中,多普勒调频率具有很高的估计精度且对场景的依赖性很小,可以更广泛地用于自聚焦处理。基于多普勒调频率参数估计,针对回波包络及相位分别提出了误差提取模型,并通过包络误差校正和相位误差补偿两个步骤实现了高精度的运动补偿处理。实测数据表明,本文方法可以在低精度导航信息情况下获取高分辨率雷达图像。     

Some aging properties of parallel and series systems with a random number of components

In this article, we study aging properties of parallel and series systems with a random number of components. We show that the decreasing likelihood ratio property is closed under the formation of random minima. We also show, by counterexamples, that other aging properties are not closed under the formation of random minima or maxima. Some mistakes in the literature are corrected. © 2014 Wiley Periodicals, Inc. Naval Research Logistics 61: 238–243, 2014     

Some comparisons of residual life of coherent systems with exchangeable components

Most of the research, on the study of the reliability properties of technical systems, assume that the components of the system operate independently. However, in real life situation, it is more reasonable to assume that there is dependency among the components of the system. In this article, we give sufficient conditions based on the signature and the joint distribution of component lifetimes to obtain stochastic ordering results for coherent and mixed systems with exchangeable components. Some stochastic orders on dynamic (or conditional) signature of coherent systems are also provided. © 2014 Wiley Periodicals, Inc. Naval Research Logistics 61: 549–556, 2014     

A general approach to the shape of failure rate and MRL functions

Failure rate and mean residual life are two important characteristics for studying reliability of products. In literature, some work studied the shape of failure rate function based on the knowledge of the associated probability density function; some other work investigated the shape of mean residual life function based on the shape of the associated failure rate function separately for continuous case and discrete case. In this article, a general approach is developed which can be applied to the aforementioned studies. © 2004 Wiley Periodicals, Inc. Naval Research Logistics, 2004     

基于四元联系数的非战争军事行动装备保障能力评价方法研究

针对非战争军事行动装备保障能力评价问题,综合运用能力模型和集对分析理论,在构建非战争军事行动装备保障能力评价指标体系基础上,建立非战争军事行动装备保障能力四元联系数评价模型,并示例说明该方法的应用．     

纯引力轨道验证质量辐射计效应与气体阻尼耦合模型的数值分析

辐射计效应和气体阻尼是纯引力轨道验证质量的重要干扰力,是影响纯引力轨道构造水平的重要因素.在纯引力轨道飞行器中,这两种力分别描述了由腔体中温度梯度和验证质量相对运动引起的气体分子作用,两者从不同角度描述了气体分子作用力,均是气体分子作用力的一部分,而两者的耦合模型则可以反映验证质量受到的气体分子作用力总和.针对耦合模型形式复杂的特点,本文以内编队系统为例,利用数值方法分析了耦合模型中的影响因素,这些因素包括内卫星相对运动速度、内卫星半径、外卫星腔体半径、腔体平均温度、腔体温差和腔体平均压力等.对大量计算结果进行了数据拟合,给出了内卫星气体分子作用力与各物理参数关系的拟合公式,和原始计算结果相比,拟合误差在20％以内.     

舰炮大型铸铝件断裂残余应力分析

采用盲孔法测试某型舰炮大型铸铝件残余应力,结果分析表明原结构中残余应力较大,部分位置残余应力超过材料屈服极限是其断裂的根本原因.通过工艺改进后,构件残余应力幅值大幅降低,满足工程要求.