用于动平衡测试的MDAC窄带跟踪滤波器

为了从强干扰噪声中提取出与转速同频的振动分量,且适应转速波动时的情形,利用互相关原理导出了跟踪滤波方法,并采用乘法数模转换器(MDAC)设计并实现了窄带跟踪滤波器。实验结果表明,其增益相对误差优于0.2%,相位绝对误差优于0.4°,当转速变化率不超过9000r/min2时,滤波器的输出能够跟踪转速的变化。该滤波器能较好地满足动平衡测试的需要。     

Testing or fault-finding for reliability growth: A missile destructive-test example

A new piece of equipment has been purchased in a lot of size m. Some of the items can be used in destructive testing before the item is put into use. Testing uncovers faults which can be removed from the remaining pieces of equipment in the lot. If t < m pieces of equipment are tested, then those that remain, m₁ = m − t, have reduced fault incidence and are more reliable than initially, but m₁ may be too small to be useful, or than is desirable. In this paper models are studied to address this question: given the lot size m, how to optimize by choice of t the effectiveness of the pieces of equipment remaining after the test. The models used are simplistic and illustrative; they can be straightforwardly improved. © 1997 John Wiley & Sons, Inc. Naval Research Logistics 44: 623–637, 1997     

长管水击最大水击压强的解析

从管道水击微分方程的特征分析入手,提出了水击特征方程的黎曼不变量和网格分析解,建立了管道水击问题的近似解析解,给出了长管水击最大水击压强的计算表达式。通过实际算例对解析解和数值解结果进行了比较。对水击微分方程的重力项也进行了讨论。     

某装甲侦察车液压升降机构液压系统分析

详细介绍了某装甲侦察车液压升降机构的工作原理和液压系统,找出了存在的一些主要问题,并阐述了解决问题的初步建议.     

飞行器动力学环境预示技术应用研究

动力学环境试验技术已被广泛应用 ,但动力学环境预示技术还没有得到很好的重视和发展。讨论了几种动力学环境预示方法的特点 ,着重研究了统计能量分析 ( SEA)方法的原理及其应用 ,并以某型号发动机长尾喷管舱为例 ,具体给出其工程分析估计过程     

导弹气动伺服弹性稳定性分析

导弹气动伺服弹性稳定性分析是导弹受控舵面设计的一个重要问题。针对防空导弹的特点 ,采用气动力导数加下洗修正的非定常气动力方法来计算其气动力。在气动弹性运动方程的建立和气动弹性环节传递函数的确定上 ,采用了传统的主模态法 ,在此基础上 ,利用乃奎斯特法对导弹进行了气动伺服弹性稳定性分析和稳定裕度分析。     

燃爆信号的小波包分析在内燃机故障诊断中的应用

在燃爆信号小波包分析的基础上介绍了内燃机的脱机故障诊断技术、小波分析的特点和具体应用方法 ,提取出了对燃爆信号的诊断判据 ,为内燃机工作状态的判断提供了一种有效方法。     

备件保障效能动态评估方法

针对目前效能评估方法多重视效能指标的静态观测值,对时序状态数据所蕴含的趋势信息关注较少的缺点,提出基于灰色聚类-粗糙集和集对分析的备件保障效能动态评估方法。针对主客观赋权方法各自的优缺点,引入依赖度和重要度的概念,建立灰色聚类-粗糙集组合赋权模型;将指标权重引入集对理论,提出集对同势、均势和反势的定义,描述备件保障效能的变化规律,构建基于马尔可夫链的集对分析动态模型。实例分析结果表明,该方法可以有效反映备件保障效能的动态变化特征,为决策者制定备件保障长期计划提供科学依据。     

Sensitivity analysis on responsive pricing and production under imperfect demand updating

This paper examines three types of sensitivity analysis on a firm's responsive pricing and responsive production strategies under imperfect demand updating. Demand has a multiplicative form where the market size updates according to a bivariate normal model. First, we show that both responsive production and responsive pricing resemble the classical pricing newsvendor with posterior demand uncertainty in terms of the optimal performance and first‐stage decision. Second, we show that the performance of responsive production is sensitive to the first‐stage decision, but responsive pricing is insensitive. This suggests that a “posterior rationale” (ie, using the optimal production decision from the classical pricing newsvendor with expected posterior uncertainty) allows a simple and near‐optimal first‐stage production heuristic for responsive pricing. However, responsive production obtains higher expected profits than responsive pricing under certain conditions. This implies that the firm's ability to calculate the first‐stage decision correctly can help determine which responsive strategy to use. Lastly, we find that the firm's performance is not sensitive to the parameter uncertainty coming from the market size, total uncertainty level and information quality, but is sensitive to uncertainty originating from the procurement cost and price‐elasticity.     

零压式高空气球球形设计与参数敏感性分析

高空气球能够为临近空间科学实验提供可靠的平台,其形状直接关系到气球制作及飞行的全过程。提出将多段打靶法与序列二次规划法结合,对零压气球完全膨胀和部分膨胀状态下的球形进行求解,并运用有限元方法对球形进行稳定性及应力应变分析,验证了所推导球形的正确性。在此基础上,对影响气球形状的关键参数进行灵敏度分析及相关运用,从定量的角度得到气球载荷、飞行高度及昼夜温差对气球形状的影响规律。