基于遗传算法的2自由度并联机构的优化设计

对一种两自由度并联机构进行精度分析,给出了机构参数的误差影响因子矩阵.以动平台姿态误差最小为目标建立了的优化目标函数,并采用遗传算法求得全局最优解.     

三自由度3-RPUR并联机构性能指标分析及优化设计

基于性能图谱对一种具有良好性能的3-RPUR并联机构性能指标进行了研究,并对机构进行了优化设计。首先建立该并联机构的空间模型,然后绘制了该机构的可达工作空间、全域条件数和全域速度的性能图谱,并对其进行了分析。根据分析结果,可以按照不同的工作需求来优化机构的结构参数。最后以将该机构应用于搬运机器人为例,基于性能图谱对该机构进行了优化设计。     

索杆混合驱动并联机构设计与工作空间分析

提出一种新型索杆混合驱动并联机构,在SolidWorks中构建整体装置模型。利用空间向量分析法推导了该机构的运动学逆解模型;分析了并联平台静止状态下受力平衡关系,建立静力学平衡方程,并在此基础上讨论了机构可控工作空间的求解方法;在给定机构运动副的约束条件下,对动平台姿态可控工作空间进行数值仿真,得到仿真图像。搭建索杆混合驱动并联机构试验平台,进行末端动平台位姿变换试验。试验结果与运动学模型和工作空间数值仿真图像对比,结果表明,动平台位姿与柔索长度的关系满足运动学反解模型,末端动平台姿态可实现工作空间仿真图像中最大姿态偏转角度。研究工作为后续机构的实际应用和性能优化奠定了一定的理论基础。     

3-UPS/S并联机构运动学分析及机构优化设计

对3-UPS/S并联机构进行了运动学分析和静力学分析,得到了该机构的运动雅可比矩阵和静力学雅可比矩阵;采用离散的方法对该机构的工作空间进行了分析;对该机构进行了基于给定工作空间的尺寸参数优化,在优化的过程中考虑了机构的奇异性、关节约束和机构几何尺寸约束等条件.     

基于Kriging模型的并联机器人机构的多目标优化设计

为了提高并联机器人机构的性能特性,对机构参数进行优化设计分析,以达到性能指标最优的目的。先对应用于盾构拼装机的并联机构进行了运动学分析,利用封闭矢量法建立了逆解方程,并在此基础上求解了表征驱动关节输入和动平台输出映射关系的雅可比矩阵。引入衡量并联机构性能的全域运动灵巧度和全域承载能力指标,并以结构参数为设计变量,性能指标为优化目标,基于Krigring近似模型,利用多岛遗传算法对并联机构进行多目标优化,最终得到Pareto解集,并选取了机构参数的最优解。结果表明,基于Kriging模型的多目标优化对机构性能有明显的改善。     

基于遗传算法3-RCR并联机器人的结构参数优化设计

确定机器人机构结构参数是并联机构优化设计的难题,因为并联机器人的机构结构参数优化属于多维,多目标和多约束条件优化问题。基于3-RCR并联机构的工作空间体积,分析了机构结构参数对工作空间体积的影响。运用坐标变换法对机构的位置反解进行求解;利用极坐标边界搜索法通过具体算例确定了机构的工作空间及其边界,以工作空间为目标利用遗传算法对机构进行了结构参数优化,获得了性能优良的结构参数,运用MATLAB软件编程得到了该并联机构的工作空间图谱。为该类并联机构的进一步研究和推广应用奠定了基础。     

DFSS算法在并联机构可靠性设计优化中的应用

以茶叶筛分机所依托的空间并联机构4-UPS-S为研究对象,对机构进行运动学分析,建立机构的雅可比矩阵,并提出了衡量机构工作性能的指标。鉴于加工误差对机构参数的不确定性造成机器人性能的影响,建立了包含不确定性因素的优化设计模型,基于多学科多目标软件IOSO NM采用DFSS优化算法对模型进行求解,使工作性能指标达到整体最优。研究结果表明,考虑不确定性的多学科多目标优化应用在并联机构中是可行的,能为并联机构的优化设计奠定理论基础。     

平移式3-PUU并联机器人的分析建模

研究了一种具有三角形平台的3-PUU并联机器人机构.通过理论分析,证明了该机构在初始位置和一般情况时,动平台只做三维平动.在该并联机构上建立坐标系,运用解析几何中的坐标变换,求出了该并联机构的位置逆解,同时通过MATLAB软件对该方法进行了仿真.     

基于遗传算法的平面运动并联机构尺度综合

针对混联运动机床开发中所采用的二自由度平面运动并联机构部分进行了深入的研究,介绍了该平面运动并联机构的组成,推导了并联机构的运动学正、逆解求解公式,并给出了速度雅可比矩阵,以雅可比矩阵条件数的倒数作为灵巧度的标准并采用全域综合灵巧度的评价方法,基于遗传算法对该机构的结构参数进行了优化,为该机构的设计开发奠定了基础。     

混合人工蜂群算法在并联机构尺度优化中的应用

以4-RUPaR并联机构为研究对象,以机构杆长为约束条件,利用解析几何中的坐标变换理论,得到其运动学反解模型,根据该模型,利用所有满足约束条件的"点集"描述并联机构定姿态工作空间大小。建立以并联机构驱动连杆长度、执行连杆长度和动平台尺寸为设计变量,以工作空间最大化作为优化目标的尺度优化模型。在求解多维优化问题时,为提高算法的搜索效率及解的质量,文中将差分进化(Differential Evolution, DE)算法融入人工蜂群(Artificial Bee Colony,ABC)算法,提出一种混合人工蜂群(Hybrid Artificial Bee Colony,HABC)算法,以增强算法的全局优化能力。应用HABC算法求解并联机构尺度优化设计,获得了较好的优化效果。     

Minimal Realization of Linear Graph Models for Multi-physics Systems

An engineering system may consist of several different types of components,belonging to such physical"domains"as mechanical,electrical,fluid,and thermal.It is t...     

INTEGRAL EQUATION METHOD＇S APPLICATION IN HOLE-EDGE STRESS OF COMPOSITE MATERIAL PLATE WITH DIFFERENT SHAPED HOLES

The strength of composite plate with different hole-shapes is always one of the most important but complicated issues in the application of the composite material. The holes will lead to mutations and discontinuity to the structure. So the hole-edge stress concentration is always a serious phenomenon. And the phenomenon makes the structure strength decrease very quickly to form dangerous weak points. Most partial damage begins from these weak points. According to the complex variable functions theory, the accurate boundary condition of composite plate with different hole-shapes is founded by conformal mapping method to settle the boundary condition problem of complex hole-shapes. Composite plate with commonly hole-shapes in engineering is studied by several complex variable stress fimction. The boundary integral equations are founded based on exact boundary conditions. Then the exact hole-edge stress analytic solution of composite plate with rectangle holes and wing manholes is resolved. Both of offset axis loadings and its influences on the stress concentration coefficient of the hole-edge are discussed. And comparisons of different loads along various offset axis on the hole-edge stress distribution of orthotropic plate with rectangle hole or wing manhole are made. It can be concluded that hole-edge with continuous variable curvatures might help to decrease the stress concentration coefficient; and smaller angle of outer load and fiber can decrease the stress peak value.     

Non-monotonic material contrast in scanning ion and scanning electron images

30 keV Ga⁺ focused ion beam induced secondary electron (iSE) imaging was used to determine the relative contrast between several materials. The iSE signal compared from C, Si, Al, Ti, Cr, Ni, Cu, Mo, Ag, and W metal layers does not decrease with an increase in target atomic number Z₂, and shows a non-monotonic relationship between contrast and Z₂. The non-monotonic relationship is attributed to periodic fluctuations of the stopping power and sputter yield inherent to the ion–solid interactions. In addition, material contrast from electron-induced secondary electron (eSE) and backscattered electron (BSE) images using scanning electron microscopy (SEM) also shows non-monotonic contrast as a function of Z₂, following the periodic behavior of the stopping power for electron–solid interactions. A comparison of the iSE and eSE results shows similar relative contrast between the metal layers, and not complementary contrast as conventionally understood. These similarities in the contrast behavior can be attributed to similarities in the periodic and non-monotonic function defined by incident particle–solid interaction theory.     

Application of Feature Extraction through Convolution Neural Networks and SVM Classifier for Robust Grading of Apples

This paper proposes a novel grading method of apples,in an automated grading device that uses convolutional neural networks to extract the size,color,texture,an...     

分布动态载荷识别的抗噪处理

针对正交多项式频域法在用多种响应对矩形薄板进行载荷识别中抗噪性较差的问题,综合运用平均法、矩阵预处理和奇异值截断法等方法对之进行改善,并引入空间映射的思想,将该方法的应用范围拓展为复杂的模型.利用仿真算例,证实了该方法具有较好的抗噪性.     

基于MELTAC-N平台的核电厂安全级DCS环网研究与测试

针对工程实践中环网通讯相关问题的处理缺乏理论基础及国产化安全级DCS平台的开发缺乏成熟经验借鉴问题,对基于MELTAC-N平台核电厂安全级DCS环网的软硬件实现进行了研究。提出了安全级DCS环网双环网冗余设计、光切换开关设计等硬件设计方法,以及以RPR协议为基础,采用全数据收发策略的软件设计方法。在CPR1000安全级DCS平台上对安全级DCS环网的可靠性及实时性进行了评价,并进行了容错能力、响应时间及响应时间稳定性测试验证实验。结果表明,基于MELTAC-N平台安全级DCS环网软硬件设计具有较好的容错能力及响应时间稳定性。     

Short-Term Relay Quality Prediction Algorithm Based on Long and Short-Term Memory

The fraction defective of semi-finished products is predicted to optimize the process of relay production lines, by which production quality and productivity ar...     

End-to-End Multiview Gesture Recognition for Autonomous Car Parking System

The use of hand gestures can be the most intuitive human-machine interaction medium.The early approaches for hand gesture recognition used device-based methods....     

The laboratory simulation of abrasive wear

Abrasive wear has long been recognised as one of the most potentially serious tribological problems facing the operators of many types of plant and machinery; several industrial surveys have indicated that wear by abrasion can be responsible for more than 50% of unscheduled machine and plant stoppages. Locating the operating point of a tribological contact in an appropriate operational ‚map’︁ can provide a useful guide to the likely nature and origins of the surface degradation experienced in use, though care must be exercised in choosing the most suitable parameters for the axes of the plot. Laboratory testing of materials and simulations of machine contacts are carried out for a number of purposes; at one level for the very practical aims of ranking candidate materials or surface hardening treatments in order of their wear resistance, or in an attempt to predict wear lives under field conditions. More fundamentally, tests may be aimed at elucidating the essential physical mechanisms of surface damage and loss, with the longer term aim of building an analytical and predictive model of the wear process itself. In many cases, component surface damage is brought about by the ingress of hard, particulate matter into machine bearing or sealing clearances. These may be running dry although, more usually, a lubricant or service fluid is present at the interface. A number of standardised wear test geometries and procedures have been established for both two- and three-body wear situations, and these are briefly described. Although abrasive wear is often modelled as following an ‚Archard’︁ equation (i.e. a linear increase in material loss with both load and time, and an inverse dependence on specimen hardness) both industrial experience and laboratory tests of particularly lubricated contacts show that this is not always the case: increasing the hardness differential in an abrasively contaminated lubricated pair may not always reduce the rate of damage to the harder surface.     

ANGULAR DISTORTION ALLOWABLE VALUE AND ASSESS METHOD OF WELD ON COKE TOWER

A graph as the new engineering method for estimate the safety of bulging deformation of coke tower is proposed. Through stresses analysis of circumferential weld of coke tower and comparing the stresses produced by pressure with heat stress of steady state, residual stress, bending stress produced by both itself weight and wind loads, it showed that the stresses produced by pressure on the angle distortion are the main factor of equivalent stress of the combined stress. After comparing four kinds of stress controlling conditions, the relation to stress with depth of angular distortion, grade of curvature of angular distortion and half of region of angular distortion has been inferred. Graph of deformation allowable value of coke tower for different condition by angular distortion and half of region of angular distortion has been plotted. The five steps for its engineering use have been explained. The lighter the grade of curvature is, the larger of bulge allowance, may be, and the bigger of depth of angular distortion may pose too. For the coke tower with a popular structure of Dg 5 400 mm×28 mm, the result by graph is nearly more than the result of two formulas formed by other research, the error is less than 7.0%. But, the graph can be easily applied to different size of angular distortion.