人参质量的典型相关识别

本文给出了利用典型相关性分析研究人参所含的化学成分与其疗效关系的方法，计算出人参化学成分药理作用的权重。     

变薄拉深的上限法分析

根据上限法原理建立了一种适用于分析变薄拉深的上限模型,包括两个用于优化上限解的独立参数。通过优化计算,变薄拉深力理论值与实验值吻合良好;用该模型研究了变薄拉深系数、凹模半锥角、原始筒形件内外径比、定径带相对长度以及内外摩擦因子等主要工艺参数对变薄拉深力的影响规律。     

飞机典型结构细节——紧固孔随机裂纹扩展分析

根据7475T761铝合金犬骨型试样在随机谱载荷作用下的试验结果,采用两种随机裂纹扩展分析的方法,即通用的和解析的分析方法,研究了飞机典型结构细节——紧固孔中疲劳裂纹扩展的概率累积损伤,给出了概率裂纹扩展轨迹、裂纹扩展损伤累积分布及裂纹超出数的概率。试验结果与预测结果的比较表明,两者十分吻合,能满足工程精度的要求,为飞机结构的耐久性和损伤容限评估提供了适用的分析手段。     

Low C/N_0 Carrier Tracking Loop Based on Optimal Estimation Algorithm in GPS Software Receivers

Suppressing jitter noises in a phase locked loop(PLL) is of great importance in order to keep precise and continuous track of global positioning system(GPS) signals characterized by low carrier-to-noise ratio(C/N0).This article proposes and analyzes an improved Kalman-filter-based PLL to process weak carrier signals in GPS software receivers.After reviewing the optimal-bandwidth-based traditional second-order PLL,a Kalman-filter-based estimation algorithm is implemented for the new PLL by decorrelating the model error noises and the measurement noises.Finally,the efficiency of this new Kalman-filter-based PLL is verified by experimental data.Compared to the traditional second-order PLL,this new PLL is in position to make correct estimation of the carrier phase differences and Doppler shifts with less overshoots and noise disturbances and keeps an effective check on the disturbances out of jitter noises in PLL.The results show that during processing normal signals,this improved PLL reduces the standard deviation from 0.010 69 cycle to 0.007 63 cycle,and for weak signal processing,the phase jitter range and the Doppler shifts can be controlled within ±17° and ±5Hz as against ±25° and ±15 Hz by the traditional PLL.     

中国模具工业的发展及现状——第十三届中国国际模具技术与设备展览会形势分析

作为制造业的一个重要领域,模具的技术水平已经成为衡量一个国家制造业水平的重要标志,并在不断发展中前行。在2010年中国国际模具技术与设备展览会即将到来之际,无论金融危机的浪潮是否已经安然度过,中国模具工业都将迎来新的发展契机。     

一种联合估计的有源校正高精度测向算法

针对存在系统误差的阵列模型,提出了一种有源标校下的联合估计测向算法。该算法把误差矩阵估计转化为误差系数估计,并采用到达角精确已知的源信号进行标校,在此基础上使用最小二乘法联合估计幅相不一致误差系数和互耦误差系数,最后使用结合误差矩阵的MUSIC算法测量信号的到达角。仿真表明,该算法仅需要3个标校源,其精度相比于无阵列误差情况下降0.05°,具有较好的工程可实现性。     

高负荷压气机叶栅分离结构及其等离子体流动控制

 为揭示高负荷压气机叶栅内部流动损失的产生机理和分布规律以及等离子体气动激励的作用机制,利用拓扑分析和数值计算方法,从计算模型的建立与验证、基准流场的分离结构和等离子体流动控制3个方面展开研究;对总压损失系数分布、拓扑结构和表面流谱与空间流线分布以及旋涡结构进行分析,并开展了激励方式的优化分析.结果表明:随着攻角的增大,固壁面拓扑结构增加了3对奇点,吸力面流向激励改变了固壁面拓扑结构.当攻角为2°时,在吸力面拓扑结构中产生了一对奇点,打断了角区分离线,并引入了一条回流再附线.叶栅流道内部有5个主要涡系,尾缘径向对涡促进流体的展向流动,并成为吸力面倒流的主要组成部分;角涡是一个独立的涡系,其强度和尺度不受等离子体气动激励的影响.吸力面流向激励可以改善叶中流场,但对角区流动作用很小;端壁横向激励可以降低角区流动损失,对叶中流场作用有限;吸力面流向与端壁横向组合激励在整个叶高范围内均可以显著抑制流动分离;端壁横向流动对角区流动分离结构的影响大于吸力面附面层的分离.吸力面流向激励的优化明显降低,而端壁横向激励和组合激励的优化保持并增强了等离子体流动的控制效果.     

Y-8飞机平尾积冰导致的飞行事故分析

平尾积冰对飞行安全影响重大.通过介绍连续两起平尾积冰导致的Y-8飞机飞行事故,分析了飞机结冰的气象条件,平尾积冰和放襟翼对平尾气动特性的影响,以及平尾积冰失速的改出方法和预防措施.     

基于飞机装配型架的气动定位器的设计

利用气动定位器解决了飞机装配型架中手动定位操作困难的问题,它将传统型架设计与气动传动、PLC控制有机结合,自动化程度高,操作安全简便,工作高效,可降低98％的劳动强度,尤其适合于定位器工作通路不好、工作位置高以及工作行程长的情况下使用,在飞机装配领域有很大的应用空间。     

Acceleration sensors based modal identification and active vibration control of flexible smart cantilever plate

Some flexible appendages of spacecrafts, such as solar panels, are cantilever plate structures. Thus, vibration problem is unavoidable when there is slewing maneuver or external disturbance excitation. Vibration of such cantilever plate structures includes coupled bending and torsional motion. Furthermore, the low amplitude vibration near the equilibrium point is very difficult to be quickly suppressed due to nonlinear factors of the hardware in the system, which is harmful to stability and attitude control accuracy. To solve these problems, acceleration sensor-based modal identification and active vibration control methods are presented for the first two bending and the first two torsional modes vibration of the cantilever plate. Optimal placements of three acceleration sensors and PZT patches actuators are performed to decouple the bending and torsional vibration of such cantilever plate for sensing and actuating, and identifications are achieved by experiments. A nonlinear control method is presented to suppress both high and low amplitude vibrations of flexible smart cantilever plate significantly. Experimental comparison researches are conducted by using acceleration proportional feedback and the presented nonlinear control algorithms. The experimental results demonstrate that the presented acceleration sensor-based methods can suppress the vibration of cantilever plate effectively.