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141.
反舰导弹纯方位发射捕捉概率计算方法 总被引:8,自引:0,他引:8
反舰导弹的纯方位发射对目标信息要求不高,在目标信息的探测越来越艰难的今天,是反舰导弹较为重要的一种发射方式,也将会成为未来海战场上常用的作战方式.介绍了反舰导弹捕捉概率的计算方法和传统纯方位发射的捕捉概率的计算方法,并从分析反舰导弹捕捉概率的计算模型和影响因素出发,指出传统的反舰导弹纯方位发射的捕捉概率计算模型存在不足,并给出了修正后的计算模型. 相似文献
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Today, many products are designed and manufactured to function for a long period of time before they fail. Determining product reliability is a great challenge to manufacturers of highly reliable products with only a relatively short period of time available for internal life testing. In particular, it may be difficult to determine optimal burn‐in parameters and characterize the residual life distribution. A promising alternative is to use data on a quality characteristic (QC) whose degradation over time can be related to product failure. Typically, product failure corresponds to the first passage time of the degradation path beyond a critical value. If degradation paths can be modeled properly, one can predict failure time and determine the life distribution without actually observing failures. In this paper, we first use a Wiener process to describe the continuous degradation path of the quality characteristic of the product. A Wiener process allows nonconstant variance and nonzero correlation among data collected at different time points. We propose a decision rule for classifying a unit as normal or weak, and give an economic model for determining the optimal termination time and other parameters of a burn‐in test. Next, we propose a method for assessing the product's lifetime distribution of the passed units. The proposed methodologies are all based only on the product's initial observed degradation data. Finally, an example of an electronic product, namely contact image scanner (CIS), is used to illustrate the proposed procedure. © 2002 Wiley Periodicals, Inc. Naval Research Logistics, 2003 相似文献
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Burn‐in is a technique to enhance reliability by eliminating weak items from a population of items having heterogeneous lifetimes. System burn‐in can improve system reliability, but the conditions for system burn‐in to be performed after component burn‐in remain a little understood mathematical challenge. To derive such conditions, we first introduce a general model of heterogeneous system lifetimes, in which the component burn‐in information and assembly problems are related to the prediction of system burn‐in. Many existing system burn‐in models become special cases and two important results are identified. First, heterogeneous system lifetimes can be understood naturally as a consequence of heterogeneous component lifetimes and heterogeneous assembly quality. Second, system burn‐in is effective if assembly quality variation in the components and connections which are arranged in series is greater than a threshold, where the threshold depends on the system structure and component failure rates. © 2003 Wiley Periodicals, Inc. Naval Research Logistics 50: 364–380, 2003. 相似文献
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Modern technology is producing high reliability products. Life testing for such products under normal use condition takes a lot of time to obtain a reasonable number of failures. In this situation a step‐stress procedure is preferred for accelerated life testing. In this paper we assume a Weibull and Lognormal model whose scale parameter depends upon the present level as well as the age at the entry in the present stress level. On the basis of that we propose a parametric model to the life distribution for step‐stress testing and suggest a suitable design to estimate the parameters involved in the model. A simulation study has been done by the proposed model based on maximum likelihood estimation. © 2003 Wiley Periodicals, Inc. Naval Research Logistics, 2003 相似文献
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基于反馈线性化的飞行器姿态运动的变结构控制方法研究 总被引:4,自引:0,他引:4
利用反馈线性化方法对飞行器姿态运动的非线性耦合进行了解耦,并对得到的线性化系统进行了变结构姿态控制系统设计,该控制系统具有优良的控制品质和鲁棒性。数字仿真结果进一步证实该方法的有效性。 相似文献
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微小卫星编队飞行轨道动力学及相对位置保持控制方法 总被引:3,自引:0,他引:3
微小卫星编队飞行是20世纪90年代中、后期出现的航天新概念,它是通过一组群聚卫星的协同工作完成相应的空间任务,具有广阔的应用前景。对微小卫星编队飞行的轨道动力学建模进行了详细研究,并应用势函数方法推导了用于卫星编队飞行相对位置保持的连续控制律及离散控制律。 相似文献