徐朝梁 中国著名直升机总设计师

在此次珠海航展上,大型民用直升机AC313的精彩表演吸引了观众热切的目光,作为总设计师,您眼中的AC313是怎样的定位?徐朝梁:AC313是借鉴原有型号平台的成功设计经验、采用成熟的先进技术、按照国际最新的适航标准、采用与国际接轨的适航审定程序自主研发的全新民用直升机,是目前国内最大吨位的直升机。     

Improved Wavelet-based Spatial Filter of Damage Imaging Method on Composite Structures

Piezoelectric sensor array-based spatial filter technology is a new promising method presented in research area of structural health monitoring (SHM) in the recent years. To apply this method to composite structures and give the actual position of dam-age, this paper proposes a spatial filter-based damage imaging method improved by complex Shannon wavelet transform. The basic principle of spatial filter is analyzed first. Then, this paper proposes a method of using complex Shannon wavelet transform to construct analytic signals of time domain signals of PZT sensors array. The analytic signals are synthesized depending on the principle of the spatial filter to give a damage imaging in the form of angle-time. A method of converting the damage imaging to the form of angle-distance is discussed. Finally, an aircraft composite oil tank is adopted to validate the damage imaging method. The validating results show that this method can recognize angle and distance of damage successfully.     

固定管板式换热器的危险工况分析和管、壳应力在设计中的作用

本文在前文的基础上,阐明危险工况(或称可能出现的危险工况)和真正危险工况之间的区别和联系,仅由操作条件只能列出危险工况而无法得出真正的危险工况,真正的危险工况不仅和操作条件有关,而且和换热器的结构条件和各部件相对尺寸有关。 根据换热器的具体结构条件、各元件相对尺寸和危险工况,管板、管子或壳体应力的最大值都有可能首先超过各自的强(刚)度校核条件。所以,在设计时不论管板、管子或壳体都应由各个危险工况求出其可能出现的最大应力值并校核满足,不能以并非最大的应力值进行校核,更不能因管子或壳体应力(特别是带有膨胀节时)绝对值较低而认为其强度不会成为问题,甚至不予计算。     

某型直升机航空电子系统地面模拟试验仿真平台研究

本文介绍了某型直升机地面模拟试验应用 RT-LAB 集成环境进行地面仿真试验的过程;并阐述了RT-LAB 仿真平台的设计思想和应用前景。     

浅谈理工类专业教师的教书育人工作

在新的历史时期，面对新世纪复杂多变的国际形势和我们面临的艰巨的历史任务，高等教育如何全面实现培养高素质人才的崇高目标，这是关系到建设有中国特色社会主义事业的命运和前途的历史性课题，教师作为人类灵魂的工程师，不失时机地寻找合适的途径做好教书育人工作，这是对教师的基本要求，也是教师的职业道德和责任。     

Article

This is a slightly edited version of the Executive Summary of a joint report on cooperation in space science produced by the Space Studies Board of the USA National Research Council and the European Space Science Committee of the European Science Foundation. Using analysis of 13 case-study missions it reviews 30 years of joint missions and makes 14 recommendations based on its findings. These include the importance of setting a scientific rationale for each mission and of ensuring that objectives are shared by engineers and others involved in it, the need for independent periodic assessments and that all agreements should specify the scope, expectations and obligations of the respective agencies and relevant partners.The USA and Europe have been cooperating in space science for more than three decades. This history of cooperation has survived significant geopolitical, economic and technological changes, such as the end of the Cold War, the pressure of budget reductions and the increasing focus on economic competition and the global marketplace. Both Europe and the USA have learned from one another and acquired a knowledge base as well as an infrastructure to implement joint missions and research activities. More importantly, the decades of cooperative space research efforts between the USA and Europe have built a community of scientists whose joint scientific exchanges have established a heritage of cooperation on both sides of the Atlantic.The scientific fruits of this heritage are plainly evident in achievements such as a signature for supermassive black holes provided by the Hubble Space Telescope (HST); the first views of the solar atmosphere and corona illuminated by the Solar and Heliospheric Observatory (SOHO); the sharing of expensive research facilities on the International Microgravity Laboratory (IML); and the impressive data on ocean altimetry from the Ocean Topography Experiment (TOPEX-POSEIDON) mission, which is significantly improving our understanding of global ocean circulation.There were no guideposts for the emergence of space science cooperation between Europe and the USA. In the process of introducing new procedures and improvements to facilitate cooperation, missteps occurred, and there were political, economic and scientific losses. This report takes stock of US–European history in cooperative space endeavors, the lessons it has demonstrated and the opportunities it suggests to enhance and improve future US–European cooperative efforts in the sciences conducted in space.     

基于Η∞和μ综合的Stewart平台柔性铰链主动杆多目标鲁棒主动振动控制(英文)

新一代空间望远镜、空间激光通信平台及其他敏感载荷要求超静力学环境,传统被动减振无法满足要求,主动振动控制是一种有效的方法,Stewart平台主被动混合隔振被广泛研究。本文分析了立方Stewart隔振器6个主动杆之间的耦合特性,建立了单个主动杆的刚弹耦合动力学模型,并在模态空间中去掉刚体模态。考虑建模不确定性及传感器噪声,利用不含刚体模态的单杆动力学模型,进行多目标Η∞和μ综合控制器设计,对于低频指向控制信号进行保持,而对高频扰动进行抑制。而后对控制器进行鲁棒稳定性测试和分析,并对控制器进行了模型降阶,最后用μ降阶控制器对标称系统进行时域仿真,并与 PI 控制器比较。结果指出μ控制器达到了低频指向信号保持和高频扰动抑制的指标要求。     

TOPOLOGY OF CONFIGURATION SPACE FOR A THREE-BODY PROBLEM

考虑了限制在球面Ｓ２上运动的三个质点的力学系统，该系统的构型空间是Ｓ２上的一个纤维丛。本文证明了这个丛的第１陈省身示性类等于－２ｃ１（γ），其中γ是复射影空间ＣＰ１＝Ｓ２上的典范线丛。这个结果蕴涵该构型空间是Ｓ２上的非平凡丛。由此又算出了它的上同调群与同伦群。此外还讨论了上述拓扑性质对于诸如平衡位置的数目，周期轨道及约化相空间等涉及系统大范围性状的影响。     

Analysis of CHARTER Applied for Yushu Earthquake Relief

Natural disasters are common threats to all human beings. With the background of global climate change, major natural disasters have occurred frequently in the last few years and caused heavy casualties with high property losses. Satellite Earth ob-servation has been playing a more and more important role in monitoring and     

大学生马克思主义信仰教育：问题与对策

本文在调查研究的基础上对大学生的马克思主义信仰状况进行了分析，找出了理性信仰感性化、信仰分布多元化、入党动机功利化、理论教育不得力等问题。问题的原因有理论教育队伍的素质与教育目标的要求不相适应，教育的方式方法与目标要求不相适应，应试教育的弊端、就业的压力与迷茫、多元信息的吸引与诱惑，马克思主义在大学生信仰中的地位悄然变化等。相应的思路与对策有切实加强师资队伍建设，切实把信仰教育纳入社会系统工程，切实加强党风廉政建设、消除腐败现象对信仰教育的负面影响，切实提高大学生信仰选择能力。