Wear-resist Electrodes for Micro-EDM

This article proposes a new type of electrode for micro-electro-discharge machining (micro-EDM), which can produce ultra fine micro components from various kinds of materials including those that cannot be processed by the silicon or the Lithographie Galvanoformung Abformung (LIGA) processings. This electrode is made by way of the electrodeposition process on the basis of the difference between the discharging performance of the electrodeposited coating and that of the matrix to ensure uniform wear of electrode bottom faces. With this electrode, micro-holes on ANK80 steel can be successfully manufactured in a short period of time. Compared to the traditional electrodes, Cu-ZrB₂ composite coating electrodes display better wear resistance on the same experimental conditions. The results disclose the prospects for this electrode to be used in producing micro components of high-aspect-ratio and 3D micro-cavities.     

Two-level optimization approach for Mars orbital long-duration,large non-coplanar rendezvous phasing maneuvers

A relative dynamics equation-set based on orbital element differences with J₂ effects is derived, based on which a two-level approach is proposed to optimize the Mars orbital rendezvous phasing with a large difference in the initial ascending node. The up-level problem uses the revolution deviation between the target spacecraft and the chaser as the design variable, and employs a linear search to find the optimum. The low-level problem uses the maneuver revolutions, locations, and impulses as the design variables, and is solved using a hybrid genetic algorithm combined with sequential quadratic programming. To improve the solution accuracy, an iteration method is developed to satisfy the terminal constraints of the absolute numerical integration trajectory. Test cases involving Mars sample return missions with large initial node differences are presented, which show that the relative dynamics, two-level optimization model, and hybrid optimization algorithm are efficient and robust. Compared with previously published results, the total velocity increment has been further reduced by utilizing this proposed approach. It is found that a five-impulse plan requires the least quantity of propellant, and a propellant-optimal minimum rendezvous duration exists for this long-duration, large non-coplanar rendezvous problem.     

国有航空制造企业岗位评价策略研究

岗位评价应用需要一定基础和环境,以A公司为例指出岗位评价应当关注其适用的局限,应用前期应建立在对企业环境充分分析的基础上,灵活应用先进的岗位评价工具,应根据企业特点设计适当的方法、程序,并提出合理的岗位评价策略的应用可以在岗位评价从设计到实施全过程对其进行科学导向,从而有效保障岗位的评价效果.     

用于飞机零部件制造装配的柔性工装数控系统(英文)

研究了柔性工装计算机数字控制(Computer numerical control,CNC)系统,该系统适于控制多种用于飞机零部件制造和装配的柔性工装设备。给出了柔性工装的机械结构分类,分析了柔性工装设备的控制需求。同时提出了一种CNC系统的硬件和软件架构,并予以实现。该系统利用配置参数描述柔性工装的机械结构。根据配置参数,CNC系统可以自动生成其控制功能和人机界面(Human machine interface,HMI)操作功能。将该CNC系统应用于某蒙皮-桁条装配柔性工装设备,结果证明了系统的有效性。     

基于属性标记的关系数据库水印方法

数据库水印是保护数据库版权的一项重要技术。针对现有数据库水印方法无法抵抗有序关系模式变换攻击(ORSM)的问题,提出了一种基于属性标记的关系数据库水印方法。首先给出了有序关系模式变换攻击的定义,然后通过分析现有关系数据库水印算法无法抵抗ORSM攻击的问题,提出一种能够抵抗ORSM攻击的水印算法ALBWM,包括水印嵌入算法(ALBWM-EM)和水印检测算法(ALBWM-DT)。实验结果表明,与传统数据库水印算法相比,ALBWM算法在不影响性能的前提下对ORSM攻击具有更好的鲁棒性。     

论全球化背景下弘扬和培育民族精神的路径选择

在全球化背景下弘扬和培育民族精神,是提升国家综合实力、维护国家主权独立和坚定社会主义信念的需要;必须重点弘扬和培育爱国精神、创新精神、开放精神和忧患意识;要在保持民族文化独立性的基础上、在继承民族优秀传统文化的过程中、在推进全面建设小康社会的实践中和在中外文化交流与互动中弘扬和培育民族精神。     

脉冲测量雷达卫星标定方法研究

对脉冲测量雷达卫星标定方法的原理和工程应用等问题进行了研究,提出了标定模型和方法,分析了雷达跟踪能力和卫星定轨保障等工程应用问题,并对标定效果进行了仿真验证。     

企业技术创新能力的系统结构协调性评价模型

企业技术创新能力是由若干要素构成的一种系统能力。各组成要素之间的协调性是反映企业技术创新能力的重要参数。本文在构建企业技术创新能力指标体系的基础上,采用统计学中的变化系数来体现各指标间的协调程度,并给出模拟实证数据作进一步说明。