变速跳频通信抗跟踪干扰性能的研究

针对常规跳频通信抗跟踪干扰能力差的问题,分析跟踪干扰原理,提出变速跳频通信。建立数学模型,在干扰容限、压制比和追踪概率方面进行理论分析,分析变速跳频通信抗跟踪干扰对误码率的性能,并用MATLAB进行仿真验证。     

基于FPGA的可变速率PSK数字解调器实现

针对QPSK变速率调制数字系统,提出了一种新的基于现场可编程门阵列(FPGA)实现方法,该系统可以支持4.88 Kb/s到2 Mb/s和更高的连续比特速率。设计采用混合乘法器、数控振荡器(NCO)和积分-梳状滤波器(CIC),并给出了系统中载波和信号恢复电路的设计结构,且可以移植到任何FPGA器件。提出的设计在Xilinx Virtex-5 FPGA平台进行了硬件测试。硬件实现结果显示,采用本方法实现的解调器,表现出优越的使用效率。     

基于战备完好率的军用飞机维修费用需求确定方法

军用飞机维修费用需求与战备完好率要求密切相关,为保持飞机一定的战备完好率水平,必须投入一定的维修费用。维修费用投入多,则维修设备齐全,维修人员维修能力高,维修备件充足,飞机故障修复时间短,战备完好率高;维修费用投入少,会造成维修设备短缺,设施破旧,维修人员培训不到位,维修备件供应不足等各种问题,直接影响战备完好率水平。     

高空动能拦截器末制导导引方法设计与实现

以高空动能拦截器为研究对象,为其末制导段设计了一种“逐段限制视线转率”的导引方法,使之最终能直接命中目标,实现动能拦截的任务并通过仿真计算验证了该导引法的可行性。     

Verification and validation of detonation modeling

The mathematical model used to describe the detonation multi-physics phenomenon is usually given by highly coupled nonlinear partial differential equations. Numerical simulation and the computer aided engineering (CAE) technique has become the third pillar of detonation research, along with theory and experiment, due to the detonation phenomenon is difficult to explain by the theoretical analysis, and the cost required to accredit the reliability of detonation products is very high, even some physical experiments of detonation are impossible. The numerical simulation technique can solve these complex problems in the real situation repeatedly and reduce the design cost and time stunningly. But the reliability of numerical simulation software and the serviceability of the computational result seriously hinders the extension, application and the self-restoration of the simulation software, restricts its independently innovational ability. This article deals with the physical modeling, numerical simulation, and software development of detonation in a unified way. Verification and validation and uncertainty quantification (V&V&UQ) is an important approach in ensuring the credibility of the modeling and simulation of detonation. V&V of detonation is based on our independently developed detonation multi-physics software-LAD2D. We propose the verification method based on mathematical theory and program function as well as availability of its program execution. Validation is executed by comparing with the experiment data. At last, we propose the future prospect of numerical simulation software and the CAE technique, and we also pay attention to the research direction of V&V&UQ.     

Dynamic signatures and their use in comparing the reliability of new and used systems

The signature of a system with independent and identically distributed (i.i.d.) component lifetimes is a vector whose ith element is the probability that the ith component failure is fatal to the system. System signatures have been found to be quite useful tools in the study and comparison of engineered systems. In this article, the theory of system signatures is extended to versions of signatures applicable in dynamic reliability settings. It is shown that, when a working used system is inspected at time t and it is noted that precisely k failures have occurred, the vector s [0,1]^n‐k whose jth element is the probability that the (k + j)th component failure is fatal to the system, for j = 1,2,2026;,n ‐ k, is a distribution‐free measure of the design of the residual system. Next, known representation and preservation theorems for system signatures are generalized to dynamic versions. Two additional applications of dynamic signatures are studied in detail. The well‐known “new better than used” (NBU) property of aging systems is extended to a uniform (UNBU) version, which compares systems when new and when used, conditional on the known number of failures. Sufficient conditions are given for a system to have the UNBU property. The application of dynamic signatures to the engineering practice of “burn‐in” is also treated. Specifically, we consider the comparison of new systems with working used systems burned‐in to a given ordered component failure time. In a reliability economics framework, we illustrate how one might compare a new system to one successfully burned‐in to the kth component failure, and we identify circumstances in which burn‐in is inferior (or is superior) to the fielding of a new system. © 2009 Wiley Periodicals, Inc. Naval Research Logistics, 2009     

稳态法测量热系数的计算方法改进研究

不良导体热系数测量普遍采用的是稳态法,但表面散热率的间接测量和样品侧面散热与漏热给测量带来一定误差,使得热系数实际测量值略微偏大。介绍了新的实验装置和实验数值计算方法,并且分析研究了样品边缘（侧面）热损失的物理模型,提出了新的数学模型和数据处理方法,纠正了这些偏差,与实验吻合较好。     

Optimal redesign decisions through failure rate estimates

To reduce the time-to-market of newly developed systems, manufacturers increasingly adopt strategies where systems are brought to market while system field reliability is still uncertain. These systems are typically sold under performance-based contracts, which incentivizes potential customers to invest in them despite reliability uncertainty. Such contracts make the manufacturer (partly) responsible for the availability of the system. Subsequently, when field reliability is lower than anticipated, the manufacturer may choose to redesign the system to avoid high contract penalties. Redesign is a costly effort which may substantially increase field reliability. Deciding when to redesign is challenging, especially because the initial failure rate estimate by the system's engineers is refined over time as failure data accrues. We propose a model that endogenizes the failure rate updating to analyze this tactical redesign decision. We study additive and multiplicative redesigns and show that the optimal policy has a control limit structure. We benchmark our optimal policy against a static counterpart numerically, and conclude that basing redesign decisions on the updated estimate of the failure rate can substantially reduce costs.     

数据驱动的复杂系统非预期故障诊断通用过程模型

提高对复杂系统非预期故障诊断能力是故障诊断领域的难点。结合非预期故障诊断内涵及基本原理,构建了一种用于复杂系统非预期故障诊断的通用过程模型。该模型采用四层递进结构,包括四个主要模型,即预期(已知)故障检测模型、预期(已知)故障识别模型、非预期(未知)故障检测模型和非预期(未知)故障识别模型。分析了各模型所包含的关键问题及其相应的实现算法,包括检测统计量的构建及评估、故障特征方向提取、故障识别器设计及故障贡献率计算。该通用过程模型规范了复杂系统非预期故障的诊断流程,明确了数据驱动的实现原理。以卫星姿态控制系统为例,验证了非预期故障诊断通用过程模型的有效性。     

低功率霍尔推力器阳极供气环工程设计关键参数仿真

为了提高低功率霍尔推力器放电通道内中性原子分布均匀性,采用有限元方法对阳极供气环关键结构参数进行优化研究。针对双腔式阳极供气环结构,重点分析了缓冲腔容积比以及缓冲腔隔板导流小孔数量等关键参数对阳极供气均匀性的影响。研究结果表明:随着缓冲腔容积比的增大,阳极供气环出气孔差异率先快速减小后趋于稳定,其中当容积率k=1.0时,平均差异率和最大差异率分别为1.77%和3.79%;隔板间导流小孔数量从8增加到14时,出气孔差异率呈现浴盆曲线特性,其中导流孔数量为10时,平均差异率和最大差异率分别为1.8%和3.8%。研究结果可为霍尔推力器阳极供气环工程设计提供理论支撑。