XNAV中的相对论效应(III)——时空测量值的坐标转换

在文献[1-3]中求得的XNAV基本方程中,时间和距离是指太阳质心系(BCRS)中的坐标量。但在实际测量中,接收机测量的时间是时钟的固有时,接收机的位置一般应以地心系(GCRS)为基准。在相对论框架内完成这两个坐标转换,使得XNAV测量方程能够直接得到应用。最后给出了完整的XNAV高精度测量方程及其在实际测量中的计算过程。     

时敏打击指挥控制技术初探

分析了时敏目标打击链,介绍了压缩打击链的主要途径,描述了图像处理、战场数据管理、武器动态分配、智能代理集成等有关时敏打击指挥控制技术,为时敏打击指挥控制系统的研究提供参考。     

基于自准直反射法的光学中心偏检测系统研究

提出了一种基于自准直反射法测量光学中心偏的检测方法,分析了其测量光学中心偏的基本原理,在此基础上设计了基于自准直反射法的光学镜组中心偏检测系统。系统采用CV-A1型CCD探测器组件,以轴向晃动≤1″、径向跳动≤1μm的高精度基准轴工作台配合PIV研华工控机进行数据采集和图像处理,系统测量精度为:角度≤2,″线度≤0.01 mm。实际应用表明,该系统适用于1.06μm激光探测系统光学镜组的在线装校及系统中心偏检测,也可用于其它光学系统中心偏的测量。     

基于时域平均的齿轮故障诊断

提出了信号时域平均处理的新算法,解决了周期截断误差对平均结果的影响,并对测取的齿轮箱齿轮故障振动信号进行了处理。实验结果表明:该方法在齿轮故障信号的处理中能够消除背景噪声的影响,取得比较理想的效果。     

非自伴情形下时滞抛物方程的惯性流形

利用Lyapunov-Perron方法在适当的谱间隙条件和适当小的时滞假设下,证明了一类非自伴算子情形下半线性时滞抛物方程惯性流形的存在性。     

A stochastic model for burn‐in procedures in accelerated environment

Burn‐in procedure is a manufacturing technique that is intended to eliminate early failures of system or product. Burning‐in a component or system means to subject it to a period of use prior to being used in field. Generally, burn‐in is considered expensive and so the length of burn‐in is typically limited. Thus, burn‐in is most often accomplished in an accelerated environment in order to shorten the burn‐in process. A new failure rate model for an accelerated burn‐in procedure, which incorporates the accelerated ageing process induced by the accelerated environmental stress, is proposed. Under a more general assumption on the shape of failure rate function of products, which includes the traditional bathtub‐shaped failure rate function as a special case, upper bounds for optimal burn‐in time will be derived. A numerical example will also be given for illustration. © 2006 Wiley Periodicals, Inc. Naval Research Logistics, 2006     

Transient analysis of Markov models of fault‐tolerant systems with deferred repair using split regenerative randomization

The (standard) randomization method is an attractive alternative for the transient analysis of continuous time Markov models. The main advantages of the method are numerical stability, well‐controlled computation error, and ability to specify the computation error in advance. However, the fact that the method can be computationally very expensive limits its applicability. In this paper, we develop a new method called split regenerative randomization, which, having the same good properties as standard randomization, can be significantly more efficient. The method covers reliability‐like models with a particular but quite general structure and requires the selection of a subset of states and a regenerative state satisfying some conditions. For a class of continuous time Markov models, model class C₂, including typical failure/repair reliability‐like models with exponential failure and repair time distributions and deferred repair, natural selections are available for both the subset of states and the regenerative state and, for those natural selections, theoretical results are available assessing the efficiency of the method in terms of “visible” model characteristics. Those results can be used to anticipate when the method can be expected to be competitive. We illustrate the application of the method using a large class C₂ model and show that for models in that class the method can indeed be significantly more efficient than previously available randomization‐based methods. © 2006 Wiley Periodicals, Inc. Naval Research Logistics, 2006     

基于ADSP21160的机载图像处理系统

为解决飞机上显示器高亮度背景下无法看清画面的问题,基于模块化设计思想,提出了以DSP AD-SP21160为核心处理器的机载视频图像数字化硬件实现方案.即将红外夜视图像和微光图像处理的算法移植到作为系统的主要数据处理单元DSP上,并使用CPLD控制时序.经调试表明,该方案成功地解决了画面的亮度、对比度等问题.     

位置随动系统动态性能自动检测研究

通过分析某型位置随动系统的组成和动态技术指标,提出了位置随动系统动态性能自动检测的设计方案和测试方法,利用信号仿真模块和基于DSP的高速数据采集与处理模块,建立了自动检测的硬件电路和软件结构,确定了测试位置随动系统的动态性能指标、测试方法和软件功能,实现了对某型位置随动系统动态性能的自动检测．     

基于最短拦截时间的异面拦截机动轨道设计与优化

本文构建了单脉冲机动在燃耗约束下的最短时间拦截轨道设计模型与求解方法,将用数学泛函求边值问题转换为高次代数方程的求解计算,并用牛顿迭代法进行快速寻根,仿真结果表明模型及算法准确、有效,满足精度要求。