Beam Dynamics Issues in an Extended Relativistic Klystron
国际自动化与计算杂志.英文版.
国际自动化与计算杂志.英文版.1.Improved Exponential Stability Criteria for Uncertain Neutral System with Nonlinear Parameter PerturbationsFang Qiu,Ban-Tong Cui2.Robust Active Suspension Design Subject to Vehicle Inertial Parameter VariationsHai-Ping Du,Nong Zhang3.Delay-dependent Non-fragile H∞ Filtering for Uncertain Fuzzy Systems Based on Switching Fuzzy Model and Piecewise Lyapunov FunctionZhi-Le Xia,Jun-Min Li,Jiang-Rong Li4.Observer-based Adaptive Iterative Learning Control for Nonlinear Systems with Time-varying DelaysWei-Sheng Chen,Rui-Hong Li,Jing Li5.H∞ Output Feedback Control for Stochastic Systems with Mode-dependent Time-varying Delays and Markovian Jump ParametersXu-Dong Zhao,Qing-Shuang Zeng6.Delay and Its Time-derivative Dependent Robust Stability of Uncertain Neutral Systems with Saturating ActuatorsFatima El Haoussi,El Houssaine Tissir7.Parallel Fuzzy P+Fuzzy I+Fuzzy D Controller:Design and Performance EvaluationVineet Kumar,A.P.Mittal8.Observers for Descriptor Systems with Slope-restricted NonlinearitiesLin-Na Zhou,Chun-Yu Yang,Qing-Ling Zhang9.Parameterized Solution to a Class of Sylvester MatrixEquationsYu-Peng Qiao,Hong-Sheng Qi,Dai-Zhan Cheng10.Indirect Adaptive Fuzzy and Impulsive Control of Nonlinear SystemsHai-Bo Jiang11.Robust Fuzzy Tracking Control for Nonlinear Networked Control Systems with Integral Quadratic ConstraintsZhi-Sheng Chen,Yong He,Min Wu12.A Power-and Coverage-aware Clustering Scheme for Wireless Sensor NetworksLiang Xue,Xin-Ping Guan,Zhi-Xin Liu,Qing-Chao Zheng13.Guaranteed Cost Active Fault-tolerant Control of Networked Control System with Packet Dropout and Transmission DelayXiao-Yuan Luo,Mei-Jie Shang,Cai-Lian Chen,Xin-Ping Guanparison of Two Novel MRAS Based Strategies for Identifying Parameters in Permanent Magnet Synchronous MotorsKan Liu,Qiao Zhang,Zi-Qiang Zhu,Jing Zhang,An-Wen Shen,Paul Stewart15.Modeling and Analysis of Scheduling for Distributed Real-time Embedded SystemsHai-Tao Zhang,Gui-Fang Wu16.Passive Steganalysis Based on Higher Order Image Statistics of Curvelet TransformS.Geetha,Siva S.Sivatha Sindhu,N.Kamaraj17.Movement Invariants-based Algorithm for Medical Image Tilt CorrectionMei-Sen Pan,Jing-Tian Tang,Xiao-Li Yang18.Target Tracking and Obstacle Avoidance for Multi-agent SystemsJing Yan,Xin-Ping Guan,Fu-Xiao Tan19.Automatic Generation of Optimally Rigid Formations Using Decentralized MethodsRui Ren,Yu-Yan Zhang,Xiao-Yuan Luo,Shao-Bao Li20.Semi-blind Adaptive Beamforming for High-throughput Quadrature Amplitude Modulation SystemsSheng Chen,Wang Yao,Lajos Hanzo21.Throughput Analysis of IEEE 802.11 Multirate WLANs with Collision Aware Rate Adaptation AlgorithmDhanasekaran Senthilkumar,A. Krishnan22.Innovative Product Design Based on Customer Requirement Weight Calculation ModelChen-Guang Guo,Yong-Xian Liu,Shou-Ming Hou,Wei Wang23.A Service Composition Approach Based on Sequence Mining for Migrating E-learning Legacy System to SOAZhuo Zhang,Dong-Dai Zhou,Hong-Ji Yang,Shao-Chun Zhong24.Modeling of Agile Intelligent Manufacturing-oriented Production Scheduling SystemZhong-Qi Sheng,Chang-Ping Tang,Ci-Xing Lv25.Estimation of Reliability and Cost Relationship for Architecture-based SoftwareHui Guan,Wei-Ru Chen,Ning Huang,Hong-Ji Yang1.A Computer-aided Design System for Framed-mould in Autoclave ProcessingTian-Guo Jin,Feng-Yang Bi2.Wear State Recognition of Drills Based on K-means Cluster and Radial Basis Function Neural NetworkXu Yang3.The Knee Joint Design and Control of Above-knee Intelligent Bionic Leg Based on Magneto-rheological DamperHua-Long Xie,Ze-Zhong Liang,Fei Li,Li-Xin Guo4.Modeling of Pneumatic Muscle with Shape Memory Alloy and Braided SleeveBin-Rui Wang,Ying-Lian Jin,Dong Wei5.Extended Object Model for Product Configuration DesignZhi-Wei Xu,Ze-Zhong Liang,Zhong-Qi Sheng6.Analysis of Sheet Metal Extrusion Process Using Finite Element MethodXin-Cun Zhuang,Hua Xiang,Zhen Zhao7.Implementation of Enterprises' Interoperation Based on OntologyXiao-Feng Di,Yu-Shun Fan8.Path Planning Approach in Unknown EnvironmentTing-Kai Wang,Quan Dang,Pei-Yuan Pan9.Sliding Mode Variable Structure Control for Visual Servoing SystemFei Li,Hua-Long Xie10.Correlation of Direct Piezoelectric Effect on EAPap under Ambient FactorsLi-Jie Zhao,Chang-Ping Tang,Peng Gong11.XML-based Data Processing in Network Supported Collaborative DesignQi Wang,Zhong-Wei Ren,Zhong-Feng Guo12.Production Management Modelling Based on MASLi He,Zheng-Hao Wang,Ke-Long Zhang13.Experimental Tests of Autonomous Ground Vehicles with PreviewCunjia Liu,Wen-Hua Chen,John Andrews14.Modelling and Remote Control of an ExcavatorYang Liu,Mohammad Shahidul Hasan,Hong-Nian Yu15.TOPSIS with Belief Structure for Group Belief Multiple Criteria Decision MakingJiang Jiang,Ying-Wu Chen,Da-Wei Tang,Yu-Wang Chen16.Video Analysis Based on Volumetric Event DetectionJing Wang,Zhi-Jie Xu17.Improving Decision Tree Performance by Exception HandlingAppavu Alias Balamurugan Subramanian,S.Pramala,B.Rajalakshmi,Ramasamy Rajaram18.Robustness Analysis of Discrete-time Indirect Model Reference Adaptive Control with Normalized Adaptive LawsQing-Zheng Gao,Xue-Jun Xie19.A Novel Lifecycle Model for Web-based Application Development in Small and Medium EnterprisesWei Huang,Ru Li,Carsten Maple,Hong-Ji Yang,David Foskett,Vince Cleaver20.Design of a Two-dimensional Recursive Filter Using the Bees AlgorithmD. T. Pham,Ebubekir Ko(c)21.Designing Genetic Regulatory Networks Using Fuzzy Petri Nets ApproachRaed I. Hamed,Syed I. Ahson,Rafat Parveen1.State of the Art and Emerging Trends in Operations and Maintenance of Offshore Oil and Gas Production Facilities: Some Experiences and ObservationsJayantha P.Liyanage2.Statistical Safety Analysis of Maintenance Management Process of Excavator UnitsLjubisa Papic,Milorad Pantelic,Joseph Aronov,Ajit Kumar Verma3.Improving Energy and Power Efficiency Using NComputing and Approaches for Predicting Reliability of Complex Computing SystemsHoang Pham,Hoang Pham Jr.4.Running Temperature and Mechanical Stability of Grease as Maintenance Parameters of Railway BearingsJan Lundberg,Aditya Parida,Peter S(o)derholm5.Subsea Maintenance Service Delivery: Mapping Factors Influencing Scheduled Service DurationEfosa Emmanuel Uyiomendo,Tore Markeset6.A Systemic Approach to Integrated E-maintenance of Large Engineering PlantsAjit Kumar Verma,A.Srividya,P.G.Ramesh7.Authentication and Access Control in RFID Based Logistics-customs Clearance Service PlatformHui-Fang Deng,Wen Deng,Han Li,Hong-Ji Yang8.Evolutionary Trajectory Planning for an Industrial RobotR.Saravanan,S.Ramabalan,C.Balamurugan,A.Subash9.Improved Exponential Stability Criteria for Recurrent Neural Networks with Time-varying Discrete and Distributed DelaysYuan-Yuan Wu,Tao Li,Yu-Qiang Wu10.An Improved Approach to Delay-dependent Robust Stabilization for Uncertain Singular Time-delay SystemsXin Sun,Qing-Ling Zhang,Chun-Yu Yang,Zhan Su,Yong-Yun Shao11.Robust Stability of Nonlinear Plants with a Non-symmetric Prandtl-Ishlinskii Hysteresis ModelChang-An Jiang,Ming-Cong Deng,Akira Inoue12.Stability Analysis of Discrete-time Systems with Additive Time-varying DelaysXian-Ming Tang,Jin-Shou Yu13.Delay-dependent Stability Analysis for Markovian Jump Systems with Interval Time-varying-delaysXu-Dong Zhao,Qing-Shuang Zeng14.H∞ Synchronization of Chaotic Systems via Delayed Feedback ControlLi Sheng,Hui-Zhong Yang15.Adaptive Fuzzy Observer Backstepping Control for a Class of Uncertain Nonlinear Systems with Unknown Time-delayShao-Cheng Tong,Ning Sheng16.Simulation-based Optimal Design of α-β-γ-δ FilterChun-Mu Wu,Paul P.Lin,Zhen-Yu Han,Shu-Rong Li17.Independent Cycle Time Assignment for Min-max SystemsWen-De Chen,Yue-Gang Tao,Hong-Nian Yu1.An Assessment Tool for Land Reuse with Artificial Intelligence MethodDieter D. Genske,Dongbin Huang,Ariane Ruff2.Interpolation of Images Using Discrete Wavelet Transform to Simulate Image Resizing as in Human VisionRohini S. Asamwar,Kishor M. Bhurchandi,Abhay S. Gandhi3.Watermarking of Digital Images in Frequency DomainSami E. I. Baba,Lala Z. Krikor,Thawar Arif,Zyad Shaaban4.An Effective Image Retrieval Mechanism Using Family-based Spatial Consistency Filtration with Object RegionJing Sun,Ying-Jie Xing5.Robust Object Tracking under Appearance Change ConditionsQi-Cong Wang,Yuan-Hao Gong,Chen-Hui Yang,Cui-Hua Li6.A Visual Attention Model for Robot Object TrackingJin-Kui Chu,Rong-Hua Li,Qing-Ying Li,Hong-Qing Wang7.SVM-based Identification and Un-calibrated Visual Servoing for Micro-manipulationXin-Han Huang,Xiang-Jin Zeng,Min Wang8.Action Control of Soccer Robots Based on Simulated Human IntelligenceTie-Jun Li,Gui-Qiang Chen,Gui-Fang Shao9.Emotional Gait Generation for a Humanoid RobotLun Xie,Zhi-Liang Wang,Wei Wang,Guo-Chen Yu10.Cultural Algorithm for Minimization of Binary Decision Diagram and Its Application in Crosstalk Fault DetectionZhong-Liang Pan,Ling Chen,Guang-Zhao Zhang11.A Novel Fuzzy Direct Torque Control System for Three-level Inverter-fed Induction MachineShu-Xi Liu,Ming-Yu Wang,Yu-Guang Chen,Shan Li12.Statistic Learning-based Defect Detection for Twill FabricsLi-Wei Han,De Xu13.Nonsaturation Throughput Enhancement of IEEE 802.11b Distributed Coordination Function for Heterogeneous Traffic under Noisy EnvironmentDhanasekaran Senthilkumar,A. Krishnan14.Structure and Dynamics of Artificial Regulatory Networks Evolved by Segmental Duplication and Divergence ModelXiang-Hong Lin,Tian-Wen Zhang15.Random Fuzzy Chance-constrained Programming Based on Adaptive Chaos Quantum Honey Bee Algorithm and Robustness AnalysisHan Xue,Xun Li,Hong-Xu Ma16.A Bit-level Text Compression Scheme Based on the ACW AlgorithmHussein A1-Bahadili,Shakir M. Hussain17.A Note on an Economic Lot-sizing Problem with Perishable Inventory and Economies of Scale Costs:Approximation Solutions and Worst Case AnalysisQing-Guo Bai,Yu-Zhong Zhang,Guang-Long Dong1.Virtual Reality: A State-of-the-Art SurveyNing-Ning Zhou,Yu-Long Deng2.Real-time Virtual Environment Signal Extraction and DenoisingUsing Programmable Graphics HardwareYang Su,Zhi-Jie Xu,Xiang-Qian Jiang3.Effective Virtual Reality Based Building Navigation Using Dynamic Loading and Path OptimizationQing-Jin Peng,Xiu-Mei Kang,Ting-Ting Zhao4.The Skin Deformation of a 3D Virtual HumanXiao-Jing Zhou,Zheng-Xu Zhao5.Technology for Simulating Crowd Evacuation BehaviorsWen-Hu Qin,Guo-Hui Su,Xiao-Na Li6.Research on Modelling Digital Paper-cut PreservationXiao-Fen Wang,Ying-Rui Liu,Wen-Sheng Zhang7.On Problems of Multicomponent System Maintenance ModellingTomasz Nowakowski,Sylwia Werbinka8.Soft Sensing Modelling Based on Optimal Selection of Secondary Variables and Its ApplicationQi Li,Cheng Shao9.Adaptive Fuzzy Dynamic Surface Control for Uncertain Nonlinear SystemsXiao-Yuan Luo,Zhi-Hao Zhu,Xin-Ping Guan10.Output Feedback for Stochastic Nonlinear Systems with Unmeasurable Inverse DynamicsXin Yu,Na Duan11.Kalman Filtering with Partial Markovian Packet LossesBao-Feng Wang,Ge Guo12.A Modified Projection Method for Linear FeasibilityProblemsYi-Ju Wang,Hong-Yu Zhang13.A Neuro-genetic Based Short-term Forecasting Framework for Network Intrusion Prediction SystemSiva S. Sivatha Sindhu,S. Geetha,M. Marikannan,A. Kannan14.New Delay-dependent Global Asymptotic Stability Condition for Hopfield Neural Networks with Time-varying DelaysGuang-Deng Zong,Jia Liu hHTTp://15.Crosscumulants Based Approaches for the Structure Identification of Volterra ModelsHouda Mathlouthi,Kamel Abederrahim,Faouzi Msahli,Gerard Favier1.Coalition Formation in Weighted Simple-majority Games under Proportional Payoff Allocation RulesZhi-Gang Cao,Xiao-Guang Yang2.Stability Analysis for Recurrent Neural Networks with Time-varying DelayYuan-Yuan Wu,Yu-Qiang Wu3.A New Type of Solution Method for the Generalized Linear Complementarity Problem over a Polyhedral ConeHong-Chun Sun,Yan-Liang Dong4.An Improved Control Algorithm for High-order Nonlinear Systems with Unmodelled DynamicsNa Duan,Fu-Nian Hu,Xin Yu5.Controller Design of High Order Nonholonomic System with Nonlinear DriftsXiu-Yun Zheng,Yu-Qiang Wu6.Directional Filter for SAR Images Based on NonsubsampledContourlet Transform and Immune Clonal SelectionXiao-Hui Yang,Li-Cheng Jiao,Deng-Feng Li7.Text Extraction and Enhancement of Binary Images Using Cellular AutomataG. Sahoo,Tapas Kumar,B.L. Rains,C.M. Bhatia8.GH2 Control for Uncertain Discrete-time-delay Fuzzy Systems Based on a Switching Fuzzy Model and Piecewise Lyapunov FunctionZhi-Le Xia,Jun-Min Li9.A New Energy Optimal Control Scheme for a Separately Excited DC Motor Based Incremental Motion DriveMilan A.Sheta,Vivek Agarwal,Paluri S.V.Nataraj10.Nonlinear Backstepping Ship Course ControllerAnna Witkowska,Roman Smierzchalski11.A New Method of Embedded Fourth Order with Four Stages to Study Raster CNN SimulationR. Ponalagusamy,S. Senthilkumar12.A Minimum-energy Path-preserving Topology Control Algorithm for Wireless Sensor NetworksJin-Zhao Lin,Xian Zhou,Yun Li13.Synchronization and Exponential Estimates of Complex Networks with Mixed Time-varying Coupling DelaysYang Dai,YunZe Cai,Xiao-Ming Xu14.Step-coordination Algorithm of Traffic Control Based on Multi-agent SystemHai-Tao Zhang,Fang Yu,Wen Li15.A Research of the Employment Problem on Common Job-seekersand GraduatesBai-Da Qu。
英语课后练习
pursue responsibility grant equip restrict distinct minimum exploit award electThe group____one of its members to be their spokesperson.Wage increases are being kept to a(n)____in many companies because of the economic depression.The engineering profession now has many____branches.Now that you're 13 you should have more sense of ____.Students usually__one or more of the subjects which they have studied at "A" level, such as Art,Drama,English,Music, etc. We need to make sure that we____our resources as fully as possible.Congress is considering measures to____the sale of cigarettes.College courses should be designed to____students with knowledge and skills to help them survive in modern society. The local government____$1.1 million so that the old theatre could be taken down and rebuilt.For his achievement in the medical field, the Mayor____him a medal of merit.elected minimum distinct are located pursue exploit restrict equip granted awardedThe organization provides information on health issues to the public____.____what the Minister says, we will learn whether the Government's thinking has advanced.I'd like to say a word or two____his proposal.In response to your advertisement in the Bedfordshire Reporter, I am writing to____the post of secretary.Our company ____a 50% increase in production this year.at largeon on the basis of in support of apply for is aiming atUnit 2annual version financial entry refugee publication detailed full-time click spotI'm absolutely sure that this dress is a cheaper____of the one we saw in that department store.The bookshelves were crowded with books and scientific____.If you want to open a file, ____twice on the icon(图标)for it.To their disappointment, the thieves were____by the police at the moment they were entering the bank.During World War II, many____fled to the United States.They've updated(更新) a lot of____in the most recent edition of the dictionary.Despite____difficulties,they did not find the life in London unpleasant.After a lot of part-time jobs, John finally got a____position.In your report, you should give a____description of the whole incident.Companies publish____reports to inform the public about the previous year's activities.version publications click spotted refugees entries financial full-time detailed annualAt the age of 29, he____a commercial property business.While she was tidying up the living room, she____her old photograph album.My doctor____me____a specialist in heart disease.He hired private investigators to____his future business partner.She only____her son's marriage long after the event.set up came across referred…to check out learnt of/learned ofcareer exhibit interview procedure profileShe is now concentrating on a/an____as a fashion designer.When I went for my first____.Police insisted that Michael did not follow the correct____in applying for a visa.We organized a/an____of recent book upon constant requests from the readers.The newspaper publishes a/an____of a leading sportsman every week.career interview procedure exhibit profileimage concerned attractive belongings define statement fascination despite necessity item Company loyalty made him turn down many____job offers.Miller's____with medieval art dates from her childhood.His____that he had nothing to do with the affair was greeted with some suspicion.There are good novelists,____the terrible flood of bad novels and poor work.The shops are well stocked with food, clothing and other consumer____.Something is worrying me, but I can't____exactly what it is.She had a clear____of how she would look in twenty years' time.The agency is more____with making arty ads than understanding its clients(客户).The dead soldier was identified only by his uniform ____and personalFood and clothing are the bare____of life.attractive fascination statement despite items define image concerned belongings necessitiesThis meeting gives us a chance to____and have a good look at our problem.By reading this book, we can____the main character's personality.I just love the fun of____in different clothes for different occasions.For advice, they____one of the school's most experienced teachers.The central services of the BBC____the local stations to some extent.step back identify with dressing up turned to/looked to feed offUnit 4beam distress grace lower destruction collision explode scatter signal crashThe driver gave a____that he was going to turn right.It was reported that 41 people were killed in a plane____in the Himalayas last week.The ship's captain radioed that it was in____.The skaters moved over the ice with a smooth, effortless____.The bomb was taken away and the soldiers____it at a safe distance from the houses.They were on their way to the Shropshire Union Canal when their car was involved in a____with a truck.The Central Bank____interest rates by 2 percent.He____a cheerful welcome as he opened the door for the distinguished guest.He used to____his toys all over the floor and I had to pick them up.The____of the world's forests concerns everyone in some way.signal crash distress grace exploded collision lowered beamed scatter destructionMarta____a box of old photographs, looking for the baby's portrait.The cost of the house may be lower than we first thought; but____it will still be beyond our reach.The struggle between the drug company and the Government over prices finally____a satisfactory settlement.She was on a plane____Moscow when she fell ill.As soon as I was____, I began to have second thoughts about leaving.combed through in any case ended in bound for on boardThe____(crew) are paid to do all the work on the ship.You’d be a fool not____(embrace) an opportunity as good as that.The horse____(rear) up when it heard the gun shot.The general election, originally____(schedule) for 29th September, is to be postponed until December.The flower show____(grace) by the presence of the Queen.crew to embrace reared scheduled was gracedpurely perceive discourage dynamics unlikely specialty reasonably sink extended actuallyThe economy in that country____deeper and deeper into crisis.My father was a historian and his____was the history of Germany.They decided to close the museum____and simply because it cost too much to run.The local government has decided on new measures to____car use in favour of public transportation.It's pretty____that they'll turn up now-it's nearly ten o'clock.The interchange of ideas aids an understanding of group____.She says it's a good film and recommends it to all her friends, though she hasn't____seen it.Stop shouting and let's discuss this____reasonably.People now____that green issues are important to our future.Kathy and Eric run this small hotel as an"____home",which should give you a good idea of the atmosphere of warmth and hospitality there.was sinking specialty purely discourage unlikelydynamics actually reasonably have perceived extendedShe____politics while she was still a college student, and was elected to the lower parliament at the age of 40.Alone in London, without friends, work, or money, Shelley____despair.There was an attempt to____more men for the police force, but not many did.The idea sounds fine, but we still need to____it____in practice.She started working on an engineering degree but____college after only a year.took a deep interest in fell into sign up tryout dropped out ofUnit 6perfection storage clap observe exclusive defend survey interview quit coverThe audience____enthusiastically at the end of the play.Torrence expects to____her title successfully in the next Olympics.Would you____your job if you inherited lots of money from your parents?Jack has spent years in the development and____of his wine-making techniques.As an advanced journalist, she has____celebrities and political leaders on her radio program for over 25 years.According to a____of 1000 city residents,garbage collection is the city service people like most.The reporter managed to get a(n)____interview with the Prime Minister.We've had to build some cupboards to give us more____space."I've always found German cars very reliable,"he____.A team of sports journalists was sent to Germany to____the 2006 World Cup.clapped defend quit perfection interviewed survey exclusive storage observed coverIf you're going swimming tomorrow morning, you can____me____, because I'll be preparing for an examination.The child seemed to____the trouble he was causing, and still laughed in spite of the mother's anger.The suspect____when he heard the footsteps behind him.It is true that____even the most talented athletes lose their motivation.A new director has been brought in to____the company____.count....out be unaware of stopped in his tracks at times turn....aroundUnit 7election pillar gross surgery reconstruction principle sway fulfill rigid optimistYou have to be a born____to be able to do this hard job and not despair.Economic____in the country must begin with the recovering of agricultural production.Her speech failed to____her colleagues into supporting the plan.I felt disgusted and wandered how I could have ever been so____.The director insisted that the conditions of the contract must be____exactly.Local government____will take place in May next year.The doctor who performed the____gave Aikman an 85% chance of full recovery by September.Mother was a____of strength to us when our situation seemed hopeless.The students complained about the____rules and regulations at the school.optimist reconstruction sway principles gross fulfilled elections surgery pillar rigidThe family crisis really____; she was a competent mother and a successful career woman at the same time.The interesting thing about him is that he is one of those who always____to be lucky no matter what they do.If the traffic plan____, it will be applied to other cities too.____; the police will soon come to rescue us.<span id=d4></span><br>It's not like Catherine to be rude; she's polite____.brought out her best turn out works out Hang in there by natureI have the____duty of telling Mrs. Jones that her son has been killed. (delightful/hateful)The report strongly____the police for filing to deal with the problem. (criticize/praise)The Capitol at Washington is where____meets. (Conference/Congress)Violence is the____of modern society. (cancer/cancel)Poor Jim! In order to pay his debts, he’s been working____hard. (tremendously/greatly)hateful criticizes Congress cancer tremendouslyUnit 8threat continual potential infect adequate vitally update distribution urban document The reason I didn't do well in my exams was that I just didn't have____time to prepare.It is____important that we get extra funding for the project.Ms. Robbins was caught delivering a copy of a confidential(机密的)____to a newspaper reporter.The quick____of the virus caused great damage to the network system across the country.Traffic noise, pollution, huge concrete buildings - how can people survive in a(n)____area!The firm has identified 60 ____customers at home and abroad.I've had____problems with this car ever since I bought it!A computer virus may hide in a computer's memory, calling up and____each of the machine's data files in turn.He says he'll stop supplies getting in, but it's just an empty____because there are many other accesses suppliers.A(n)____version of the software will be available within six months.adequate vitally document distribution urban potential continual infecting threat updatedWhen the boxer____his guard, he was knocked out by the opponent.In the intelligent interview the applicant____being extremely intelligent.____his____was the vague idea that he had met her before.I check my email box every evening____.We spent all Saturday morning____the dormitory.let down came across as In the back of....mind as a matter of course cleaning up。
基于实际影响线的移动车辆过桥动力放大系数计算方法
第51卷第7期2020年7月中南大学学报(自然科学版)Journal of Central South University(Science and Technology)V ol.51No.7Jul.2020基于实际影响线的移动车辆过桥动力放大系数计算方法王宁波,周逸,周德(中南大学土木工程学院,湖南长沙,410075)摘要:通过分析现有桥梁动力放大系数(DAF)计算方法的特点和不足,提出一种基于实际影响线的DAF计算方法。
首先,从移动车辆荷载作用所致的桥梁动力响应中提取桥梁测点实际影响线;然后,引入轮胎−路面接触力分布模型,结合车轴信息并采用影响线叠加重构桥梁准静态响应;最后,提取桥梁最大静力响应并以此计算DAF。
开展移动车辆过桥数值仿真,对比研究波峰−波谷法、低通滤波法和本文基于实际影响线DAF提取方法对桥梁最大静力响应及DAF的计算差异。
研究结果表明:基于实际影响线重构法提取的桥梁最大静力响应恒定,行车速度和路面状况的改变对车辆作用下桥梁最大静态响应值提取无影响,与实际情况相符;与现有桥梁动力放大系数计算方法相比,本文方法所得DAF更加精确、合理可靠。
关键词:动力放大系数;准静态响应;响应重构;桥梁影响线中图分类号:TV45文献标志码:A开放科学(资源服务)标识码(OSID)文章编号:1672-7207(2020)07-1853-09A calculation method for moving vehicle induced bridge dynamicamplification factor based on influence lineWANG Ningbo,ZHOU Yi,ZHOU De(School of Civil Engineering,Central South University,Changsha410075,China)Abstract:The characteristics and disadvantages of the existing bridge dynamic amplification factor(DAF) calculation methods were analyzed,and a new DAF calculation method based on the influence line information of bridge structures was proposed.Firstly,the actual influence line of the measurement point on bridge was extracted from the dynamic response excited by a passing vehicle.Then,a numerical model of the tire−pavement contact force distribution and the axle information of the passing vehicle were introduced in the influence line to reconstruct the quasi-static response of the bridge.Finally,the maximum static response was extracted from the reconstructed curve to calculate the DAF.Numerical simulation of the vehicle-bridge model was conducted to compare the difference of the maximum static responses and the DAF based on the peak-valley method,low−pass filtering method and the proposed method.The results show that the maximum static response obtained by the proposed method in the paper is stable and not affected by the vehicle velocity and road pared to DOI:10.11817/j.issn.1672-7207.2020.07.011收稿日期:2019−10−12;修回日期:2019−12−22基金项目(Foundation item):国家自然科学基金资助项目(51508576,51478472);国家重点研发计划项目(2017YFB1201204) (Projects(51508576,51478472)supported by the National Natural Science Foundation of China;Project(2017YFB1201204) supported by the National Key Research and Development Program of China)第51卷中南大学学报(自然科学版)the existing bridge DAF calculation methods,the influence line based method proposed in the paper is more accurate,reasonable and reliable.Key words:dynamic amplification factor;quasi-static response;response reconstruction;bridge influence line移动车辆荷载引起的桥梁动力放大系数(dynamic amplification factor,DAF,用FDA表示)是与桥梁设计、检测评估、运营管养密切相关的重要参数,精确的FDA取值可同时反映桥梁设计的经济性和安全性。
Transportation Research Part C Emerging Technologies
Transient dynamic analysis of a floating beam–water interactionsystem excited by the impact of a landing beam Original ResearchArticleJournal of Sound and Vibration, Volume 303, Issues 1-2, 5 June2007, Pages 371-390J.Z. Jin, J.T. XingClose preview | Related articles | Related reference w ork articlesAbstract | Figures/Tables | ReferencesAbstractAn aircraft, idealised as an elastic beam with supporting system, lands with speed on anaircraft carrier or floating airport. The floating platform is idealised as a flexible beam floatingin an infinite water domain. The water is assumed incompressible and inviscid. The surface disturbance satisfies a linear free surface wave condition and an undisturbed condition atinfinity. A mathematical model is developed to describe this complex fluid–structureinteractive dynamical system, which exhibits strong coupling between the system'scomponents. An effective numerical scheme is established assuming that the two beam-likestructures are two solid substructures with motions represented by their respective modefunctions and the infinite fluid domain is modelled by a boundary element scheme. A mixedmode function-boundary element method is developed to solve the transient dynamics of thesystem in terms of the time histories of the beam displacement responses and waterpressure. The presented data demonstrates the applicability of the developed mathematicalmodel and numerical approach and some insights of the complex interactive processexhibited by the system.A rticle Outline1. Introduction2. Governing equations2.1. Fluid domain2.2. Landing beam2.3. Floating beam2.4. Fluid–structure interaction interface conditionPurchase$ 31.502.5. Initial conditions3. Mode equations of solid substructures3.1. Mode functions of a free –free beam3.2. Mode equation of landing beam3.3. Mode equation of floating beam4. Boundary element equation of the fluid domain5.Mixed mode function-boundary element equations6. Numerical solution7. Numerical results7.1. A simulation for a car running test7.2. An example simulating aircraft landing impacts8. ConclusionsAcknowledgements Appendix A. AppendixReferences427 Influence of modelling and solution methods on the FE-simulation of the post-buckling behaviour ofstiffened aircraft fuselage panels Original ResearchArticleComposite Structures , Volume 73, Issue 2, May 2006,Pages 229-236P. Linde, A. Schulz, W. RustClose preview | Related articles | Related reference w ork articles Abstract | Figures/Tables | ReferencesAbstractStiffened fuselage panels with laminated constructions play an increasing rolein aircraft design. The static behaviour through the buckling- and post-bucklingregime until failure has to be established. Apart from analytical calculations,experimental tests for different load combinations are indespensible, both ofwhich are expensive and time consuming.Purchase $ 31.50The virtual testing described here is based on a development project aiming at reducing the amount of experimental tests, and narrowing the numerical predictions to experimental results.A tool developed for parametric modelling and simulation of test shells is discussed.The numerical model is based on layered shell elements in ANSYS and for special purposes in LS-DYNA. It is outlined how far the behaviour of laminates (interaction of different and anisotropic materials, delamination and splices) can be simulated in this context.Results are given for welded panels and for fibre metal laminate panels. Comparison with experimental data is made. Recommendations for future research is provided.A rticle Outline1. Introduction1.1. General1.2. Objective1.3. Scope2. Model2.1. Geometry model2.2. Model for implicit analysis2.3. Model for explicit analysis2.4. FE-model for LS-DYNA2.5. Splices2.6. Delaminations2.7. Boundary conditions3. Computation 3.1. General 3.2. Static solution3.3. Implicit dynamic solution3.4. Explicit dynamic solution4. Results5. Summary, conclusions5.1.Summary5.2. Conclusions5.3. RecommendationsAcknowledgementsReferences428 Extratropical case study of stratosphere –troposphere exchange using multivariate analyses from mozaicaircraft data Original Research ArticleAtmospheric Environment , Volume 39, Issue 35,November 2005, Pages 6537-6549François Borchi, Emmanouil Oikonomou, Alain Marenco Close preview | Related articles | Related reference w ork articlesAbstract | Figures/Tables | ReferencesAbstractA multivariate analysis methodology, applied to ozone, water vapour andpotential temperature data collected from MOZAIC aircraft allowed to identifyand to quantify three types of air masses directly linked tostratosphere-troposphere exchanges (STE). These air masses occurred inFebruary 1997 over the North Atlantic during the development of a Rossbywave, which is manifested in the form of four different structures, namelytrough, ridge, streamer and cut-off low (COL). Here a study is conducted on 20isobaric (i.e. at 230 hPa) flights crossing all these upper-level structures. It isshown that the first type of air mass corresponds to a mixed zone between thePurchase $ 35.95stratosphere and the troposphere when the tropopause is poorly defined and when there exist medium values and weak gradients of ozone, potential temperature and humidity. The second type of air mass reveals an irreversible transport from the troposphere to the stratosphere for all these structuresl eading to a ―wet‖ stratosphere with high values of water vapour. The third type of air mass corresponds to the classical stratosphere with high values of ozone and low values of water vapour. The comparison with the model results of Kowol-Santen et al. (2000) shows that these first two air masses are directly linked to either diabatic processes or turbulent diffusion depending on the orientation and the type of the structure. The western side of the trough (with no mixing zone on the eastern side) and the ridge are dominated by clear air turbulence (CAT). On the other hand, the decay of the COL seems to be the result of strong convection on its northern and eastern flanks. Concerning the decay of the streamer, it is found to be due to both diabatic and turbulent processes. The above results suggest that the existence of a mixing zone during STE seems to be a more realistic concept instead of that where the tropopause is considered as a surface.A rticle Outline1. Introduction2. The MOZAIC database3. Methodology of MA4. Evolution of a trough structure in February 19975. Air masses in the trough, ridge, COL and streamer structures5.1. The trough and ridge structures5.2. The COL structure5.3. The streamer structure6. Discussion and comparison with model result of KS007. Conclusions Acknowledgements References429 Adaptive actuator failure compensation for nonlinearMIMO systems with an aircraft controlapplication Original Research ArticleAutomatica, Volume 43, Issue 11, November 2007,Pages1869-1883Xidong Tang, Gang Tao, Suresh M. JoshiClose preview | Related articles | Related reference w ork articlesAbstract | Figures/Tables | ReferencesAbstractA direct adaptive approach is developed for control of a class of multi-inputmulti-output (MIMO) nonlinear systems in the presence of uncertain failures ofredundant actuators. An adaptive failure compensation controller is designedwhich is capable of accommodating uncertainties in actuator failure timeinstants, values and patterns. A realistic situation is studied with fixed groupingof actuators and proportional actuation within actuator groups. The adaptivecontrol system is analyzed, to show its desired stability and asymptotictracking properties in the presence of actuator failure uncertainties. As anapplication, such an adaptive controller is used for actuator failurecompensation of a twin otter aircraft longitudinal model, with design conditionsverified and control structure and adaptive laws developed for a nonlinearaircraft dynamic model. The effectiveness of adaptive failure compensation is demonstrated by simulation results.A rticle Outline1. Introduction2. Problem statementPurchase$ 35.953. Adaptive failure compensation design4. Application to aircraft flight control5. ConclusionsReferencesVitae430 An aircraft acquisition decision model under stochastic demand Original Research ArticleJournal of King Saud University - Science, In Press, Corrected Proof, Available online 28 December 2010Hooi Ling Khoo, Lay Eng TeohClose preview | PDF (445 K) | Related artic les | Related reference w orkarticlesAbstract | Figures/Tables | ReferencesAbstractThis study proposes the probabilistic dynamic programming model to address the stochastic demand issue in aircraft acquisition problem. A probable phenomena is defined to comprehend the uncertain state variables so that the targeted level of service could be achieved profitably by the airline company. The objective function and the constraints have a linear expression with respect to the decision variables, and hence the proposed model is then converted as a linear programming model. The proposed model and the solution method are then examined with an illustrative case study to determine the number and the types of new aircraft that should be purchased at every time period. The results show that the proposed methodology is viable in providing the optimal solution.A rticle Outline1. Introduction2. Nomenclature3. Problem formulation3.1. Probabilistic dynamic programming model3.1.1. Stage, state variables and optimal decision3.1.2. Constraints3.1.3. Objective function3.1.4. The probable phenomena, s 1, … , s k3.1.5.The optimization model4. Solution method5. An illustrative case study5.1. Benchmark scenario5.1.1. Other scenarios6. Results and discussion7. Conclusions References431 Aerodynamic seal for reduction of noise generated on aircraft control surfacesSealing Technology , Volume 2009, Issue 2, February2009, Page 13Close preview | Related articles | Related reference w ork articles Abstract | Figures/TablesNo abstract is available for this article. Purchase $ 31.50432 Partial substitution of hydrogen for conventional fuel in an aircraft by utilizing unused cargo compartmentspace Original Research ArticleInternational Journal of Hydrogen Energy , Volume 35,Issue 3, February 2010, Pages 1463-1473Enis T. Turgut, Marc A. Rosen Close preview | Related articles | Related reference w ork articles Abstract | Figures/Tables | ReferencesAbstractOptions are being actively sought in aviation to switch from petroleum-based fuels to alternative fuels, of which hydrogen is a promising candidate, despite challenges associated with its production and storage. The possibility is Purchase $ 31.50demonstrated in this study of using hydrogen in place of some mission fuel without making substantial aircraft modifications and while utilizing only available unused baggage space in the lower-deck cargo compartments of aircraft. The environmental impact reduction and weight increase are obtained accounting for a broad range of factors including aircraft model, seat capacity, passenger and baggage load factors, annual landing and take off cycles, container type, and costs of metal hydride and gaseous hydrogen storage units of various sizes. It is found that, while there may be a cost increase, CO2 emissions are substantially reduced, by 25,000–570,000 tonnes annually in several cases and by up to 1.1 million tonnes annually for the 10 types of aircraft considered. It is also determined that with present technology, despite the low density of hydrogen, the weight of storage systems constitutes more of a challenge than their volume in aviation. Large-body aircraft are found to have more difficulties than the narrow-body aircraft regarding storage system weight. For the most frequently used narrow- and large-body aircraft considered, the number of the available containers within the required limits of weight and volume respectively are found to be 3 and 4 for the B 737-800 aircraft and 2 and 10 for the A 340-300 aircraft. Overall, the combined usage of hydrogen and kerosene investigated here may be feasible in the future, but is a challenging option with present technology and aircraft due to various factors.A rticle OutlineNomenclature1. Introduction2. Approach3. Hydrogen storage4. Lower-deck hydrogen storage5. Results and discussion 5.1. Case study 15.2. Case study 26. ConclusionsAcknowledgementsAppendixReferencesVitae433Noise radiation of aircraft panels subjected toboundary layer pressure fluctuationsOriginal ResearchArticleJournal of Sound and Vibration, Volume 314, Issues 3-5,22 July 2008, Pages 693-711Bilong LiuClose preview | Related articles | Related reference w ork articlesAbstract | Figures/Tables | ReferencesAbstractIn this paper, a method which predicts the sound radiation of aircraft panelssubjected to turbulent boundary layer excitation is described. The method isthe extension of an earlier deterministic approach, where the modal expansionand modal receptance methods were used to predict random noisetransmission through curved aircraft panels with stringer and ring frameattachments. Here, with implementation of the Corcos and Efimtsov models tocharacterize the dynamic surface pressure cross-spectra, closed-formsolutions for the panel displacements, radiation and transmission pressuresare derived. Numerical examples are presented to illustrate the effects of thestringers, ring frames, hydrodynamic coincidence, curvature, in-plane tension,structural dissipation and composite material on the structural and acousticresponse of the panel.Purchase$ 31.50A rticle Outline1. Introduction2. TBL-induced noise for a rectangular panel with stringer attachments2.1. Governing equations and velocity response2.2. Slightly curved panels with stringer attachments2.3. The radiated power spectrum3. Numerical study3.1. Solution for a typical aircraft panel3.2. Effects of the ring frame attachments3.3. Effects of the stringer attachments3.4. Damping influence3.5. Curvature and in-plane tension influence3.6. Metallic panel vs composite panel4.Concluding remarksAcknowledgementsAppendix A. The modal excitation termsReferences434 A computational study of Benders decomposition for the integrated aircraft routing and crew schedulingproblem Original Research Article Computers & Operations Research , Volume 32, Issue 6, June 2005, Pages 1451-1476Anne Mercier, Jean-François Cordeau, François Soumis Close preview | Related articles | Related reference w ork articles Abstract | Figures/Tables | ReferencesAbstractThe integrated aircraft routing and crew scheduling problem consists indetermining a minimum-cost set of aircraft routes and crew pairings such that Purchase$ 31.50each flight leg is covered by one aircraft and one crew, and side constraints are satisfied. While some side constraints involve only crews or aircraft, linking constraints impose minimum connection times for crews that depend on aircraft connections. We propose an enhanced model incorporating robustness to handle these linking constraints and compare two Benders decomposition methods—one with the aircraft routing problem as the master problem and one with the crew pairing problem. We also study the impact of generating Pareto-optimal cuts on the speed of convergence of these methods. Computational experiments performed on test instances provided by two major airlines show that the proposed approach yields high-quality solutions in reasonable computing times.A rticle Outline0. Introduction1. Mathematical formulation1.1. Aircraft routing networks1.2. Crew pairing networks1.3. Model2. Solution methodology2.1. Benders decomposition using the crew pairing problem as a master problem2.1.1. Three-phase algorithm2.2. Identifying strong cuts2.3. Step-by-step description of the improved algorithm3. Computational experiments3.1. Description of data sets3.2. Summary of computational experiments3.3. Comparisons with the extended crew pairing approach of Cohn andBarnhart [2]4. Conclusion AcknowledgementsReferences435Sample preparation and characterization of artificiallyaged aircraft coatings for microstructuralanalysis Original Research ArticleMaterials Characterization, Volume 55, Issue 3,September 2005, Pages 179-189Lisa M. Farrier, Stephen L. SzarugaClose preview | Related articles | Related reference work articlesAbstract | Figures/Tables | ReferencesAbstractThe paper describes a method for metallographic preparation of artificiallyaged aircraft coatings. In order to better understand the in-serviceperformance and identify degradation mechanisms of an aircraft coating,complete characterization of the microstructure is essential. This paperdiscusses metallographic sample preparation and subsequent microscopytechniques (light optical microscopy, scanning electron microscopy) forcharacterization of a standard polyurethane aircraft coating system. Thepreparation method has proven to produce good, consistent results on a widerange of laboratory-produced simulated environmental exposures.The military specification coating system under study (MIL-PRF-85285C andMIL-PRF-23377G) degrades severely after accelerated weathering. Typicaldegradation includes deterioration of the polyurethane-based resin system inthe topcoat and is observed as a visible change in the color. Increasedporosity and some physical deterioration were also observed. In addition,some inorganic pigments in the primer appear to migrate into the topcoatPurchase$ 31.50during simulated exposure.A rticle Outline1. Introduction2.Experiment procedure2.1. Coating application2.2. Proposed metallographic method2.3. Method justification3. Results and discussion3.1. Microstructural characterization3.2. Free film transmissivity4. SummaryAcknowledgementsReferences436 Intelligent adaptive nonlinear flight control for a high performance aircraft with neural networksOriginal Research ArticleISA Transactions , Volume 45, Issue 2, April 2006, Pages 225-247Aydogan Savran, Ramazan Tasaltin, Yasar Becerikli Close preview | Related articles | Related reference w ork articles Abstract | ReferencesAbstractThis paper describes the development of a neural network (NN) based adaptive flight control system for a high performance aircraft. The main contribution of this work is that the proposed control system is able to compensate the system uncertainties, adapt to the changes in flightconditions, and accommodate the system failures. The underlying study can be considered in two phases. The objective of the first phase is to model the Purchase$ 31.50dynamic behavior of a nonlinear F-16 model using NNs. Therefore aNN-based adaptive identification model is developed for three angular rates of the aircraft. An on-line training procedure is developed to adapt the changes in the system dynamics and improve the identification accuracy. In thisprocedure, a first-in first-out stack is used to store a certain history of theinput-output data. The training is performed over the whole data in the stack atevery stage. To speed up the convergence rate and enhance the accuracy forachieving the on-line learning, the Levenberg-Marquardt optimization methodwith a trust region approach is adapted to train the NNs. The objective of thesecond phase is to develop intelligent flight controllers. A NN-based adaptivePID control scheme that is composed of an em ulator NN, an estimator NN,and a discrete time PID controller is developed. The emulator NN is used tocalculate the system Jacobian required to train the estimator NN. Theestimator NN, which is trained on-line by propagating the output error throughthe emulator, is used to adjust the PID gains. The NN-based adaptive PIDcontrol system is applied to control three angular rates of the nonlinear F-16model. The body-axis pitch, roll, and yaw rates are fed back via the PIDcontrollers to the elevator, aileron, and rudder actuators, respectively. Theresulting control system has learning, adaptation, and fault-tolerant abilities. Itavoids the storage and interpolation requirements for the too many controllerparameters of a typical flight control system. Performance of the controlsystem is successfully tested by performing several six-degrees-of-freedomnonlinear simulations.437An integrated aircraft routing, crew scheduling andflight retiming model Original Research ArticleComputers & Operations Research, Volume 34, Issue 8,August 2007, Pages 2251-2265Anne Mercier, François SoumisClose preview | Related articles | Related reference w ork articlesAbstract | Figures/Tables | ReferencesPurchase$ 31.50AbstractIn the integrated aircraft routing, crew scheduling and flight retiming problem, a minimum-cost set of aircraft routes and crew pairings must be constructed while choosing a departure time for each flight leg within a given time window. Linking constraints ensure that the same schedule is chosen for both the aircraft routes and the crew pairings, and impose minimum connection times for crews that depend on aircraft connections and departure times. We propose a compact formulation of the problem and a Benders decomposition method with a dynamic constraint generation procedure to solve it. Computational experiments performed on test instances provided by two major airlines show that allowing some flexibility on the departure times within an integrated model yields significant cost savings while ensuring the feasibility of the resulting aircraft routes and crew pairings.A rticle Outline0. Introduction1. Mathematical formulation1.1. Model1.2. A simpler formulation2. Solution methodology2.1. Benders decomposition2.1.1. Three-phase algorithm2.1.2. Dynamic constraint generation3. Computational experiments3.1. Description of data sets3.2. Summary of computational experiments4. ConclusionAcknowledgements References438 Low-crested coastal defence structures as artificialhabitats for marine life: Using ecological criteria indesign Original Research ArticleCoastal Engineering, Volume 52, Issues 10-11,November2005, Pages 1053-1071P.S. Moschella, M. Abbiati, P. Åberg, L. Airoldi, J.M.Anderson, F. Bacchiocchi, F. Bulleri, G.E. Dinesen, M.Frost, E. Gacia, L. Granhag, P.R. Jonsson, M.P. Satta, A.Sundelöf, R.C. Thompson, S.J. HawkinsClose preview | Related articles | Related reference w ork articlesAbstract | Figures/Tables | ReferencesAbstractCoastal defence structures to protect sedimentary coastlines from erosion andflooding are increasingly common throughout Europe. They will become more widespread over the next 10–30 years in response to rising and stormier seasand accelerating economic development of the coastal zone. Building coastaldefences results in the loss and fragmentation of sedimentary habitats andtheir replacement by artificial rocky habitats that become colonised by algaeand marine animals. The engineering design and construction of thesestructures have received considerable attention. However, the ecologicalconsequences of coastal defences have been less extensively investigated. Furthermore, due to their rapid proliferation, there is a growing need tounderstand the role of these man-made habitats in the coastal ecosystems inorder to implement impact minimisation and/or mitigation measures.As part of the DELOS project, targeted studies were carried out throughoutEurope to assess the ecological similarity of low-crested coastal defencestructures (LCS) to natural rocky shores and to investigate the influence ofLCS design features on the colonising marine epibiota. LCSs can bePurchase$ 35.95considered as a relatively poor surrogate of natural rocky shores. Epibiotic communities were qualitatively similar to those on natural rocky shores as both habitats are regulated by the same physical and biological factors. However, there were quantitative differences in the diversity and abundance of epibiota on artificial structures. Typically, epibiotic assemblages were less diverse than rocky shore communities. Also, LCSs offered less structurally complex habitats for colonisation and in some locations experienced higher disturbance than natural shores. We propose several criteria that can be integrated into the design and construction of LCSs to minimise ecological impacts and allow targeted management of diversity and natural living resources.A rticle Outline1. Introduction2. Material and methods2.1. Study sites and general methodological approach2.2. Comparison of diversity between low crested structures and natural rocky shores2.3. Effects of LCS design features on epibiotic assemblages2.3.1. Orientation2.3.2. Location on the shore2.3.3. Habitat complexity2.3.4. Disturbance: structural stability and scouring of LCS3. Results3.1. Epibiota of LCSs versus rocky shore communities3.2. Effects of LCS design features on epibiota3.2.1. Orientation3.2.2. Location on the shore (tidal height)3.2.3. Habitat complexity3.2.4. Disturbance: structural stability and scouring4. Discussion 4.1. Can LCSs be viewed as artificial rocky shores?4.2. Influence of engineering design on epibiota: what can and cannot be modified5. ConclusionsAcknowledgementsReferences439 Carbon fiber reinforced plastics in aircraft constructionOriginal Research ArticleMaterials Science and Engineering: A , Volume 412, Issues1-2, 5 December 2005, Pages 171-176 C. Soutis Show preview | Related articles | Related reference w ork articles Purchase $ 41.95440Vibration-based skin damage statistical detection and restoration assessment in a stiffened aircraftpanel Original Research Article Mechanical Systems and Signal Processing , Volume 22,Issue 2, February 2008, Pages 315-337D.D. Rizos, S.D. Fassois, Z.P. Marioli-Riga, A.N. Karanika Show preview | Related articles | Related reference w ork articlesPurchase$ 35.95 441Estimation of directivity and sound power levels emitted by aircrafts during taxiing, for outdoor noiseprediction purpose Original Research Article Applied Acoustics , Volume 68, Issue 10, October 2007, Pages 1263-1279C. Asensio, I. Pavón, M. Ruiz, R. Pagan, M. Recuero Show preview | Related articles | Related reference w ork articles Purchase$ 41.95 442Strategic planning in fractional aircraft ownership programs Original Research ArticleEuropean Journal of Operational Research , Volume 189,Issue 2, 1 September 2008, Pages 526-539Yufeng Yao, Özlem Ergun, Ellis Johnson, William Schultz, J.M. Singleton Show preview | Related articles | Related reference w ork articlesPurchase $ 31.50。
基于ABAQUS梁单元的钢筋混凝土框架结构数值模拟
基于ABAQUS梁单元的钢筋混凝土框架结构数值模拟一、本文概述Overview of this article本文旨在探讨基于ABAQUS梁单元的钢筋混凝土框架结构数值模拟。
文章将对钢筋混凝土框架结构进行简要介绍,阐述其在实际工程中的应用及其重要性。
接着,将详细介绍ABAQUS软件及其在结构数值模拟中的优势,特别是梁单元在模拟钢筋混凝土框架中的应用。
This article aims to explore the numerical simulation of reinforced concrete frame structures based on ABAQUS beam elements. The article will provide a brief introduction to reinforced concrete frame structures, explaining their application and importance in practical engineering. Next, we will provide a detailed introduction to ABAQUS software and its advantages in structural numerical simulation, especially the application of beam elements in simulating reinforced concrete frames.文章将重点分析使用ABAQUS软件建立钢筋混凝土框架结构的数值模型的过程,包括材料属性的定义、边界条件的设置、荷载的施加以及网格的划分等。
还将探讨如何对模拟结果进行分析和评估,以便更好地理解和预测钢筋混凝土框架结构的性能。
The article will focus on analyzing the process of establishing a numerical model of reinforced concrete frame structures using ABAQUS software, including the definition of material properties, setting of boundary conditions, application of loads, and meshing. We will also explore how to analyze and evaluate simulation results in order to better understand and predict the performance of reinforced concrete frame structures.通过本文的研究,旨在为工程师和研究者提供一种有效的数值模拟方法,以便在设计和优化钢筋混凝土框架结构时,能够更准确地预测其受力性能和变形行为。
7. PERFORMING ORGANIZATION NAME(S) AND ADDRESS(ES)
6. AUTHOR(S)
M. D. Williams
8. PERFORMING ORGANIZATION REPORT NUMBER
7. PERFORMING ORGANIZATION NAME(S) AND ADDRESS(ES)
NASA Langley Research Center Hamptቤተ መጻሕፍቲ ባይዱn, VA 23665-5225
A02
Unclassi ed
Standard Form 298(Rev. 2-89)
Prescribed by ANSI Std. Z39-18 298-102 NASA-Langley, 1992
A technology for transmitting high power by laser beam over large distances using a quasi-coherent array of lasers is described. This technology achieves quasi-coherency by turning OFF selected laser elements, rather than trying to correct their phase as present technologies do. Such an array puts less power into a speci ed area in the far eld than a fully coherent array but gains two major advantages: (1) laser array elements are greatly simpli ed and less expensive and (2) array lifetime can be lengthened. The degree of coherency can be chosen. The greater the coherency, the greater is the lifetime of the array (for a speci ed power transmission requirement). More laser elements remain inactive. Also, by making array element selection a dynamic process, the technology can actively correct any phase changes induced in the array. The technology is analyzed, results of a computer experiment are presented, and a laboratory experiment for further development of the technology is proposed. For many years, NASA has studied the transmission of power by laser beam (refs. 1 and 2), with potential applications identi ed both in space and on Earth. Such applications require high power (up to megawatts) di raction limited laser systems. One method to obtain such systems is to assemble arrays of less powerful lasers which can be scaled to the laser power required. Arrays also lend themselves to building the large apertures required for transmission over large distances. The larger the transmission aperture is, the smaller the received laser spot size for a given range. Arrays have usually been described in terms of their ultimate power transmission capability (i.e., the maximum power that a coherent array could transmit into a speci ed area in the far eld). Coherent arrays transmit optical amplitudes that are in phase in space and time. Although coherent arrays are feasible, they are very di cult to obtain in practice. They require complex and expensive electro-optical components that are still challenged by the dynamics of a real system (i.e., heat distribution, alignment, mechanical stress). Thus, the questions arise: \Is the power transmission loss due to incomplete coherence worth the cost of obtaining complete coherence?" and \Are there other advantages of a partially coherent array?" These questions have led to an idea labeled \dynamic selection of emitting laser array elements." This idea represents a new approach to obtaining concentrated laser power in the far eld. In this approach, laser array elements are not \forced" to be perfect (coherent) but are simply turned OFF
无人驾驶英语作文80词
无人驾驶英语作文1Unmanned driving is a revolutionary technology that is transforming the way we travel. The basic principle of unmanned driving lies in the combination of various advanced technologies, such as sensors and algorithms.Sensors play a crucial role. They include cameras, lidar, and radar, which constantly collect information about the surrounding environment. These sensors can detect obstacles, other vehicles, pedestrians, and road signs. The collected data is then processed by complex algorithms. These algorithms analyze the information and make decisions on how the vehicle should move, accelerate, brake, or change lanes.Let's take some mainstream car brands as examples. Tesla's Autopilot system allows for semi-autonomous driving on highways. It can maintain a safe distance from the vehicle in front, adjust speed automatically, and even change lanes when the driver gives the command. Another example is Waymo, which has been testing fully autonomous vehicles in specific areas. Their technology enables the vehicle to navigate through complex urban environments.In conclusion, unmanned driving holds great promise for improving road safety and increasing travel efficiency. However, there are stillchallenges to be overcome, such as ensuring the reliability of the technology and addressing legal and ethical issues. But with continuous advancements, we can expect unmanned driving to become more common in the future.2Unmanned driving, a revolutionary technology that holds great promise for the future of transportation, also brings along numerous challenges. One of the most significant issues is determining legal liability in case of accidents. For instance, if an unmanned vehicle collides with another vehicle or causes harm to pedestrians, it is often difficult to attribute responsibility clearly. Is it the fault of the vehicle's manufacturer, the software developers, or some other party?Another complex problem is the moral dilemma. Imagine a situation where an unmanned vehicle has to make a split-second decision to avoid an accident. It might have to choose between hitting a group of pedestrians or swerving into a barrier, potentially causing harm to the passengers. How should such decisions be programmed and who decides the ethical guidelines?There have been several controversial incidents related to unmanned driving. In one case, an unmanned car failed to recognize a pedestrian crossing the road and resulted in a serious accident. This raised questions about the reliability and effectiveness of the vehicle's sensors andalgorithms.To address these challenges, clear and comprehensive laws and regulations need to be established. Manufacturers and developers should be held accountable for the safety and performance of their products. Advanced technologies such as better sensors, improved algorithms, and enhanced machine learning capabilities should be employed to improve the decision-making ability of unmanned vehicles. Moreover, public awareness and education about unmanned driving are crucial to ensure acceptance and understanding of this technology.In conclusion, while unmanned driving offers exciting possibilities, it is essential to overcome the challenges through a combination of legal measures, technological advancements, and public engagement. Only then can we fully realize the benefits of this transformative technology.3Unmanned driving is set to revolutionize transportation and our lives in the future in numerous ways. Firstly, it will significantly reduce traffic accidents. Human errors, such as distractions, fatigue, and speeding, are major causes of accidents. However, with unmanned driving, vehicles are controlled by advanced sensors and algorithms that can react instantly and precisely, minimizing the risk of crashes. For instance, in emergency situations, the unmanned system can make much quicker and more accurate decisions than a human driver.Secondly, unmanned driving will greatly enhance travel efficiency. Autonomous vehicles can communicate with each other and traffic infrastructure in real-time, optimizing routes and avoiding traffic congestion. Imagine a future where commutes are smooth and predictable, and people can use the time spent in the vehicle for productive activities like working or relaxing.In addition, new transportation models will emerge. We might see unmanned shuttles operating in specific areas, providing on-demand transportation services. Or perhaps unmanned delivery vehicles will become common, ensuring packages are delivered promptly and accurately. Moreover, unmanned taxis could offer shared rides, reducing the number of private cars on the road and further easing traffic pressure.In conclusion, unmanned driving holds immense potential to transform our transportation systems and improve our quality of life. While there are challenges to overcome, the benefits it brings are undeniable and exciting.4When it comes to the comparison between driverless cars and traditional ones, there are several notable aspects to consider. Firstly, in terms of comfort, driverless cars have a clear advantage. Imagine sitting in a driverless vehicle, where you can freely adjust your seat to the most relaxing position, and enjoy various entertainment options without thedistraction of the driver's maneuvers. For instance, on a recent journey in a driverless car, I was able to peacefully read a book and listen to my favorite music without any sudden jerks or stops.However, traditional driving also has its merits. The sense of control and the immediate response to road situations can give drivers a certain level of satisfaction. I remember a time when driving a traditional car on a winding mountain road, the thrill of handling the curves and the engine's roar beneath me made the experience quite exciting.In terms of safety, driverless cars are equipped with advanced sensors and algorithms that can potentially avoid human errors. They can react swiftly to unexpected obstacles. But traditional driving relies on the driver's vigilance and experience. Sometimes, a skilled driver can make split-second decisions that might even surpass the capabilities of the pre-programmed systems.To sum up, both driverless and traditional driving have their unique features and drawbacks. The choice between them depends on personal preferences and specific circumstances. As technology progresses, we can expect further improvements in both to enhance our transportation experiences.5The development of driverless technology is a remarkable advancement in the modern era. With the rapid progress of science andtechnology, this field is evolving at an astonishing pace. The integration of 5G technology has brought about revolutionary changes to driverless systems. The high-speed and low-latency characteristics of 5G enable real-time data transmission, allowing vehicles to respond promptly to various road conditions and obstacles.The global market for driverless technology holds immense potential. It is predicted that by a certain year, a significant percentage of new vehicles sold worldwide will incorporate at least some level of autonomous driving features. For instance, major automotive companies and tech giants are investing heavily in research and development. Some have achieved breakthroughs in areas such as sensor accuracy and algorithm optimization, which greatly enhance the safety and reliability of driverless cars.However, despite these promising developments, there are still challenges to overcome. Issues such as legal and ethical considerations, as well as public acceptance, need to be addressed. But with continuous innovation and collaboration among industries, the future of driverless technology looks bright. It has the potential to transform not only the transportation sector but also our daily lives, making travel more efficient, comfortable, and safe.。
最新版本工程应用英语
工程应用英语课程一.单选题:1. Computers are(B. useless)unless they are given clear and accurate instructions and information.2. Active (B. Recruiting) for engineers often begins before the student’s last year in the university.3. For the student who is preparing to become a (C. Civilengineer), these specialized courses may deal with such subjects as geodetic surveying, soil mechanics.4. The civil engineer may work in research, design, construction,(B. Supervision), maintenance, or even in sales.5. Civil engineers work on many different kinds of (C. Structures).6. In designing buildings, civil engineers often work as (B. Consultants) to architectural or construction firms.7. Dams, bridges and other large projects ordinarily employ several engineers whose work is coordinated by a (D. Systems) engineer who is in charge of the entire project.8. Construction is a(B. Complicated) process on almost all engineering projects.9. In compression, the material is (C. Pushed) together.10. When a saw cuts easily through a piece of wood, the wood is (A. in tension).11. We defined (D. Shear) as the tendency of a material to fracture along the lines of stress.12. The principal construction materials of earlier times were wood and (C. masonry brick),stone, or tile, and similar materials.13. Modern cement is a mixture of(B. limestone and clay).14. Concrete is very (D. Versatile) 15. Steel has great tensile strength whileconcrete has great compressive strength,thus, the two substances (C. Complement)each other.16. One system that helps (A. Cut)concrete weight to some extent usespolymers.17. The retention money serves to insure(D. the employer)against any defects thatmay arise in the work.18. The civil engineering work must becompleted to the satisfaction of theemployer, or his(D. Representative)19. For moderate and longer hauls,self-loading scrapers pulled byrubber-tired hauling units and push-loadedby tractors offer(B. Lower) cost.20. Highway maintenance activities canbe grouped and classified according (D.to)the purpose of the treatment.21. Engineering is a profession, whichmeans that an engineer must have aspecialized(D.university )education.22. In most cases, the tender maybe(B.Withdrawn)at any time until it hasbeen accepted.23. Current trend is to require students totake courses in the(C.social)science andthe language arts.24. The law relating to contracts imposeson each party to a contract (D. a legalobligation) to perform.25. Indeed, the civil engineer’s choiceis(C. large)and varied.26. Roadbeds (B. underlie) highwaypavement structures and the ballast andtrack on which trains move.27. Construction can be very (A.dangerous).28. Where material is moved less thanabout 60m or steeply downhill, driftingwith a track or wheel type bulldozer is (A.cheapest)29. Thrust is the pressure exerted by eachpart of a structure on (A. its other part)30. The weight of all the people, cars,furniture, and machines and so on that thestructure will support when it is in use is(B. live load)31. In tension, the material is(B. pulledapart)32. In fills constructed by end dumping orby placing in thick layers, material,density, and moisture content could (C.vary) greatly from one spot to another.33. Both (A. steel and cement), the twomost important construction materials ofmodern times, were introduced in thenineteenth century.34. The total station is used to measureangles in both vertical and horizontalplanes, and the level to measure (C.elevation difference)35. The (B. defective )vehicle is a creatorof accidents.36. Prestressed concrete is an (B.improved )form of reinforcement.37.A simple contract consists of anagreement entered into by( D. two ormore parties)38.(B. V olume) change would result indifferential settlement or swell betweenadjacent areas.39. There are two basic procedures forcontrolling the embankment density:‘manner and method’ and ‘(A. result )’.40.A main source of accidents, theproblem of(C. drunken)driving is the mostserious of all.41. Computer programming is nowincluded in almost all engineering(B.curricula).42. The relationship between engineeringand society is getting( C. Closer)43. Types of contracts are virtually classified by their(D. payment)system: (1) price-based and (2) cost-based.44. Computers can’t solve complicated problems unless they are given( D. a good program)45. In recent years, rippers have been used successfully to( C. break up)loose or fractured rock.46. Civil engineering projects are almost always (A. distinctive)47. Usually there are (C. no)easy answers on equipment selection.48. (A. Vertical)force acts up and down.49. Layered construction also produced greater uniformity in the material( D. itself)and in its density and moisture content.50. The actual cost of any single highway traffic accident is extremely( C. difficult )to determine.51. Basically, causes of automobile accidents can be categorized(D. into)four major groups.52. Electronic distance measuring (EDM) not only can measure the distance between objects but also determine( A. the direction)53.(A. Two of )the recent improvement in visibility are wraparound windshields and narrowed roof support pillars.54. There is a great deal that the actual highway designer can( C. do to)prevent accident.55. To avoid the driving after drinking, one of the methods is( B. breath test ). 56. It is suitable for remote sensing technique to be used for highway location in(C. mountainous country without forest).57. The information on the aerial photographs can be converted into mapswith the help of stereoscopes which isable to see objects in(C. three dimensions)58. The normal steel does not exert anyforce of its own on the member,( B.contrary)to the action of prestressingsteel.59. The extensive use of prestressedstructures has been due in ( A. no )smallmeasures to the advances in thetechnology.60.The employer selects the contractor forthe project by( D. Bidding).61. Many different( A. corporations ) andgovernment agencies have competed forthe services of engineers in recent years.62. Civil engineers may prefer to workwith one of the government agenciesthat( B. deals )with water resources.63. It is normal practice for( B. a)engineerto specialize in just one kind.64. Construction involves the work andutilizing the equipment and the materialsso that costs are kept as( C. low )aspossible.65. For example, (B. dams)are often builtin wild river valleys or gorges.66. Electrical and mechanical engineerswork on the(A. design )of the powerhouseand its equipment.67. In Rome, most of the people livedin(B. insulse ), great tenement blocks thatwere often ten stories high.68. The prospective civil engineer shouldbe aware of the physical( A.Conditions)that will be made on him orher.69. Much of the work of civil engineeringis carried on( C. outdoors)70. In addition, the building ofskyscrapers, bridges and tunnels must alsoprogress under all kinds of(C.weather)conditions.71. The Romans also used a naturalcement called pozzolana, made from (B.volcanic ash), that became as hard asstone under water.72. Different proportions of theingredients produce concrete with( A.different )strength and weight.73. (A. Prestressed) concrete has made itpossible to develop buildings with unusualshapes.74. The modern engineer must alsounderstand the (C. different)stresses towhich the materials in a structure aresubject.75. Today, scientific data permit theengineer to make careful calculations( D.in advance)76. The force which the live load will beexerted on the structure is( C. Impact)77. When a saw begins to bind, the woodis( A. in compression because)the fibersin it are being pushed together.78. ( D. Steel )rods are bent into theshapes to give them the necessary degreeof tensile strength.79. Many great buildings built in earlierages are massive structures with( B. thickstone walls)80. We all enter into contracts almostevery day for the supply f goods,(Btransportation)etc.81. Some contracts must be made in aparticular(D. form)to be enforceable.82. Once a person has signed a documenthe is assumed to have(B. approved)itscontents.83. By setting down the terms of acontract in writing one secures avoiding( A. disputes)84. In an entire contract, where( D. theemployer)agrees to pay a certain sum inreturn for civil engineering work..85. (B. The contractor ) is not entitled to any payment if he abandons the work prior to completion.86. The contractor is not entitled to receive payment in (A. full )until the work is satisfactorily completed.87. A tender is normally required to be a definite( C. offer)88. Generally, civil engineering contracts provide for the issue of (B. interim certificates)at various stages of the works.89. It does not give the employer the right to demand an(A. unusually)high standard of quality throughout the works.90. The employer does not usually bind himself to accept the lowest or indeed any tender and this is often stated in the(C. advertisement )91. A contract has been defined as an agreement which directly creates and contemplates( C. an obligation)92. When we enter into contracts we are willing to(C. pay )for the service we receive.93. If there is no written agreement and( C.a dispute )arises in respect of the contract.94. The rubber-tired tractor units have difficulty in operating on( D. wet), slippery roadbeds.95. There are( A. Many)variables in earthmoving.96. The term(D. Embankment)describes the fill added above the low points along the roadway to raise the level to the bottom of the pavement structure.97. Material for( B. embankment)commonly comes from roadway cuts or designated borrow areas.98.(C. Field) control is largely a matter of conducting the specified procedure.99. Modern practice requires that embankment construction be( A.carefully )executed and controlled.100. Construction of pavement over highfills often was( B. deferred )for a year ormore after completion of the fill to allowthe settlement to occur.101. Nearly( B. all)vegetable mattershould be removed from the originalground and fill material.102. A track or wheel type bulldozer is( D.not suitable)to earthmoving ofconsiderably long hauls.103. Loose rock is handled by( A.tractor-scraper)units as is done with‘common’ excavation.104. The highway can require mentaland( A. physical) response.105. The needs generated by the greatincrease( D. in)vehicle numbers andkilometers of road have given rise tomajor research programs in trafficplanning.106. Terminology concerned( B.with)highway preservation variesconsiderably from country to country.107. Highway improvement is also a keyfactor( B. in) preventing accidents.108. The actual degree of safety oneexperiences on a given highway isdetermined by decisions made on ( B.different) levels.109. Public agencies typically dictate themajor constraints within which thesedesign decisions are( A. to be) made.110. Finally, individual motorists makedecisions regarding their own safety ( C.as) they select speed, route for their cars.111. Safe highways are ( C. expensive)and it appears that the driving public doesnot want safe highways.112. People do not want to pay the costsand suffer the restrictions necessary toproduce ( A. safety) in traffic.113. It is often ( A. impossible)todetermine the true condition of a vehicleafter a crash.114. No figures( B. are)available tojustify it.115. For the driver’s vision, in the body ofthe automobile, both side and rearwindows have been greatly( D. enlarged)in area.116. Another improvement in drivervisibility is the introduction of theremote-controlled( B. outside)rearviewmirror.117. The safe performance of the brakesystem( C. under)high temperatures hasbeen ensured.118. Relocation and reduction in theheight of the brake pedal has meant thatthe brake can be applied( A. much)rapidly.119. The use of uniform traffic controldevices will reduce driver reactiontime( A. as well as) confusion.120. Removal, relocation and redesign offixed obstructions, can provide a clear( C.recovery) area for vehicles out of control.121. Vehicular safety design usuallycenters( B. upon) protecting the driver andhis passengers.122. The highway construction may alsocause( D. adverse)impacts on thesurroundings.123. The designed highway alignmentmust meet the technical( B. standard)ofthe highway engineering.124.( A. Hot rolled asphalt)is a gapgraded material with less coarseaggregate.125. In this case, layer thickness, moisturecontrol, and the number of passes by aroller of specified type and weight are( A.predetermined).126.( B. Ground survey)is the conventional location technique for highway.127. A( B. total station)is only used for measuring the vertical heights of objects. 128. If Party A commissions Party B to execute the construction work, then Party B is referred to as( B. the contractor). 129. The force-account work should be checked and approved daily by( D. both A and B) .130.( A. Fast speed)is not advantage of highway transportation.二.填空题:131. Engineers often work as( consultants)to architectural or construction firms.132. Young engineers may choose to go into( environmental)or sanitary engineering.133. It is sufficient in order to create a legally( binding), if the parties express their agreement and intention to enter into such a contract.134. One party to the contract is( liable)for breach of contract if he fails to perform his part of the agreement. 135.( Clearing)the site precedes all grading and most other construction operations.136. Loose rock includes materials such as( rotten or weathered)rock, or earth mixed with boulders.137. No attempt was made to control( moisture)content or to secure compaction.138. The( redesign)of windshield wipers, fresh air ventilating systems, had result in greater vehicle safety.139. The safe performance of the brake system has been ensured by the use of( heavy-duty)brake fluid.140. Relocation and reduction in height ofthe brake( pedal)has meant that thedriver’s total reaction time has beenreduced.141. Areas of research connected withcivil engineering include soil mechanicsand ( soil stabilization) techniques.142. Modern cement, called ( Portlandcement), was invented in 1824.143. Material for embankment commonlycomes from roadway cuts or designated( borrow areas).144. Causes of automobile accidents canbe categorized into four major groups: thevehicles, the road, the driver, the( pedestrain) .145. Another improvement in drivervisibility is the introduction of theremote-controlled outside ( rearview)mirror.146. Rock nearly always must be drilledand blasted, then loaded with a front-endloader or ( power shovel)into trucks orother hauling units.147. The three forces that can act on astructure are( vertical force), horizontalforce, and those that act upon it with arotating or turning motion.148. Highway pavements are divided intotwo main categories: ( rigid) and flexible.149. Flexible pavements are furtherdivided into three subgroups: high type,( intermediate), and low type.150. The constructing steps of thetransportation system are to plan, design,build, operate and ( maintain).151. The unit price contract is adapted tohighway engineering, because usually it isnot possible to determine exact quantitiesof some items of work ( before)construction is completed.152. The word ‘contract’is derived fromthe Latin ‘contractum’, meaning( drawn)together.153. As a structural material, theenormous advantage of steel is its ( tensilestrength).154. ( Highway transportation)is thedominant transportation mode inpassenger travel.155. The Portland cement concretecommonly used for rigid pavementsconsists of Portland cement, coarseaggregate, ( fine aggregate), water.156. Rigid highway pavement can bedivided into three general types: plainconcrete pavements, simply reinforcedconcrete and ( continuously reinforcedconcrete)pavements.157. The simplest and generally leastcostly form of interchange is the( diamond).158. If distances are great and time is at apremium, ( air)transportation will beselected.159. Signing for freeways should beplanned concurrently with the ( geometry)design.160. Major drainage structures are usuallylarge bridges and multi-span ( culverts).161. The weight of the structure itself isknown as( dead load).162.( Prestressed) concrete is an improvedform of reinforcement.163. A simple contract consists ofan( agreement)entered into by two ormore parties.164. This sum is known as ‘( retention)money’ and serves to insure the employeragainst any defects that may arise in thework.165. Thus,( On-the-job )training can beacquired to translate theory into practiceto the supervisors.166. Large projects ordinarily employ several engineers whose work is coordinated by a( systems engineer). 167. Traffic loads are transferred by the wearing surface to the underlying supporting materials through the interlocking of aggregates, the frictional effect of( granular materials), and cohesion of the fine materials.168. Excavation is the process of loosening and removing earth or rock and transporting it to a fill or to a( waste deposit).169. When planning a structure, an engineer must take into account four factors: dead load,( live load), impact and safety factor.170. The new design standards require( guard)rails and other structures to lessen a vehicle’s impact.171. People select( air transportation)to carry important goods when time is at a premium.172. The benefit-cost ratio method is used for evaluating the( economical)and environmental feasibility of the alternative routes.173. A unique bridge site or a mountain pass also mat become a primary( control point ).174. The radius of a tangent is( infinite), and that of a curve is finite.ing collector-distributor roads can overcome weaving movement of the( cloverleaf) interchange.三.阅读理解题:Passage OneResearch is one of the most important aspects of scientific and engineering practice. A researcher usually works as a member of a team with other scientistsand engineers. He or she is oftenemployed in a laboratory that is financedby government or industry. Areas ofresearch connected with civil engineeringinclude soil mechanics and soilstabilization techniques, and also thedevelopment and the testing of newstructural materials.176. Research is one of ( B. the mostimportant)aspects of scientific andengineering practice.177. A researcher is often employed( C. ina laboratory).178. A researcher usually works as amember of a team with( C. scientists andengineers).179. Which of the following is true?(A.Civil engineering research doesn’t includeonly soil mechanics and soil stabilization,but also the development of new structuralmaterials)Passage TwoThe current tendency is to develop lightermaterials. Aluminum, for example, weighsmuch less than steel but has many of thesame properties. Aluminum beams havealready been used for bridge constructionand for the framework of a few buildings.Attempts are also being made to produceconcrete with more strength and durability,and with a lighter weight. One system thathelps cut concrete weight to some extentuses polymers, which are long chainlikecompounds used in plastics, as part of themixture.180. The current trend of structuralmaterials is( B. to develop lightermaterials).181. Aluminum weighs( A. much less thansteel).182. Aluminum has( C. many of the sameproperties of steel) .183. Which of the following is true?(B.Aluminum beams can be used for not onlybridge construction but also theframework of a few buildings)Passage ThreeSteel and concrete also complement eachother in another way: they have almost thesame rate of contraction and expansion.They therefore can work together insituations where both compression andtension are factors. Steel rods areembedded in concrete to make reinforcedconcrete in concrete beams or structureswhere tension will develop. Concrete andsteel also form such a strong bonds—theforce that unites them—that the steelcannot slip within the concrete. Stillanother advantage is that steel does notrust in concrete. Acid corrodes steel,whereas concrete has an alkaline chemicalreaction, the opposite of acid.184. Steel and concrete have( C. almostthe same rate of contraction andexpansion).185. Reinforced concrete is( A. steel rodswhich are embedded in concrete beams).186. Which of the following is true?(C.steel does not rust in concrete)187. Concrete has( B. an alkalinechemical reaction, the opposite of acid).Passage FourThe employer or promoter of civilengineering works normally determinesthe conditions of contract, which definethe obligations and performances by someform of competitive tendering and anycontractor who submits a successfultender and subsequently enters into acontract is deemed in law to havevoluntarily accepted the conditions of contract adopted by the promoter.The obligations that a contractor accepts when he submits a tender are determined by the form of the invitation to tender. In most cases the tender may be withdrawn at any time until it has been accepted and may, even then, be withdrawn if the acceptance is stated by the promoter to be ‘subject to formal contract’ as is often the case.188. The conditions of contract are normally determined by( C. the promoter). 189. This conditions define the obligations and performances to which (C. the contractor) will be subject.190. The obligations that( C. the contractor)accepts when he submits a tender are determined by the form of the invitation to the tender.191. In most cases the tender may be withdrawn at any time until( B. it has been accepted) .Passage FiveMaterials are usually described as ‘rock’, ‘loose rock’, or ‘common’, with ‘common’signifying all material not otherwise classified. Rock, sometimes called ‘solid rock’, nearly always must be drilled and blasted, then loaded with a front-end loader or power shovel into trucks or other hauling units. Blasted rock may be moved or drifted for short distances by means of a bulldozer, which is, in effect, a huge tractor-mounted blade. Loose rock often is dug with loaders or shovels without any previous blasting. 192. According to the passage, which material signifying all material not otherwise classified.( B. common)193. Which of the following is NOT true?( B. rock, is sometimes called ‘looserock’)194. According to the passage, which ofthe following is true?( B. loose rock isoften dug without any previous blasting)195. Loose rock often is dug with( B.loaders or shovels)without any previousblasting.Passage SixIn the university, mathematics, physics,and chemistry are heavily emphasizedthroughout the engineering curriculum,but particularly in the first two or threeyears. Mathematics is very important inall branches of engineering, so it is greatlystressed. Today, mathematics includescourses in statistics, which deals withgathering, classifying, and usingnumerical data, or pieces of information.An important aspect of statisticalmathematics is probability, which dealswith what may happen when there aredifferent factors, or variables, that canchange the results of a problem. Beforethe construction of a bridge is undertaken,for example, a statistical study is made ofthe amount of traffic the bridge will beexpected to handle. In the design of thebridge, variables such as water pressureon the foundations, impact, the effects ofdifferent wind forces, and many otherfactors must be considered.196. Mathematics is very important in allbranches of engineering so( A. it is greatlystressed).197. Statistics deals with( B. gathering,classifying and using pieces ofinformation).198. An important aspect of statisticalmathematics is( A. probability) .199. Which is the main meaning of thepassage?( B. mathematics is veryimportant in all branches of engineering)Passage SevenCivil engineering projects are almostunique; that is, each has its own problemsand design features. Therefore, carefulstudy is given to each project even beforedesign work begins. The study includes asurvey both of topography and subsoilfeatures of the proposed site. It alsoincludes a consideration of possiblealternatives, such as a concrete gravitydam or an earth-fill embankment dam.The economic factors involved in each ofthe possible alternatives must also beweighed. Today, a study usually includes aconsideration of the environmental impactof the project. Many engineers, usuallyworking as a team that includes surveyors,specialists in soil mechanics, and expertsin design and construction, are involved inmaking these feasibility studies.200. Civil engineering projects are ( A.almost always distinctive)201. Each project( C. must be studiedcarefully)before design work begins202. The study, which must consider notonly structural features but also economicfactors and possible alternatives or otherchoices, is called( B. feasibility study) .203. Which of the following is true?(A.today civil engineering project needconsider the environmental impact of theproject )Passage EightClearing the site precedes all grading andmost other construction operations. Siteclearing in rural areas may sometimesmerely require that glass, shrubs, andother plants or crops be removed.However, it sometimes can involve removing trees and tree stumps and disposing of the debris. The accepted procedure is to remove practically all vegetable matter from the original ground and from fill material, since, if allowed to remain; it may decay and leave voids that result in settlement. Selective clearing in adjoining areas may at times be required. 204. According to the passage, which is the main topic?( B. site clearing)205. According to the passage, ( B. crops) is NOT be removed in rural areas.206. If all vegetable remained,( C. it may decay and leave voids).207. Sometimes it is required clearing( A. adjacent areas) .Passage NineVehicular safety design usually centers on protecting the driver and his passengers in case an accident occurs due to some other failure in the highway system. Examples of this type of design are safety belts and shoulder harnesses, safer door latches, non-shattering windshields, and energy absorbing steering columns. Improvements are made constantly in the parts of a vehicle which are obvious to the driver. These parts include windshield wipers, headlamps, brakes, steering suspension, and the exhaust system. The introduction of front and rear directional signals contributes greatly to motor vehicle safety. Stop lights, backup lights, and four-way emergency flashers also aid in vehicle safety. Four-way emergency flashers have become standard equipment for vehicles.208. According to the passage, which is NOT mentioned?( C. brake pedal)209. According to the passage, which becomes standard equipment forvehicles?( A. four-way emergencyflashers)210. Which of the following is true?( B.Vehicular safety design usually centers onprotecting the passengers and the personswho drives the vehicles)211. According to the passage, whichdesign is described?( A. vehicular safety)Passage TenIn the 1930s engineers found that superiorembankments could be constructed byspreading the material in relatively thinlayers and compacting it at moisturecontent close to optimum. Theimprovement resulted largely becausegreater density was obtained, whichresulted in higher “strength”in the soilmass and in decreased settlement andrutting. Layered construction alsoproduced greater uniformity in thematerial itself and in its density andmoisture content. This was beneficialsince any subsequent consolidation orswelling would be relatively uniform.212. In the 1930s engineers foundembankments could be constructed by( B.compacting it at a moisture content andspreading the material in relatively thinlayers)213. According to the passage, whichcause higher “strength”?( A. greaterdensity was obtained)214. Which of the following is true?( C.layered construction produced greaterunanimity in its density and moisturecontent)215. Which of the following words is theclosest meaning of ‘optimum’?( B. best)Passage ElevenAltogether, three forces can act on astructure: vertical—those that act up ordown; horizontal—those that act sideway;and those that act upon it with a rotatingor turning motion. Forces that act at anangle are combination of horizontal andvertical forces. Since the structuresdesigned by civil engineers are intendedto be stationary or stable, these forcesmust be kept in balance. The verticalforces, for example, must be equal to eachother. If a beam supports a load above, thebeam itself must have sufficient strengthto counterbalance that weight. Thehorizontal forces must also equal eachother so that there is not too much thrusteither to the right or to the left. And forcesthat might pull the structure around mustbe countered with forces that pull in theopposite direction.216. Horizontal forces( B. act sideways).217. Forces acting at an angle arecombination of( A. horizontal and verticalforces).218. The horizontal forces must equaleach other so that( C. there is not toomuch thrust either to the right or to theleft).219. Which of the following is true?( B.three forces acting on a structure must bekept in balance)Passage TwelveWe all enter into contracts almost everyday for the supply of goods, transportationand similar service, and in all theseinstances we are quite willing to pay forthe services we receive. Our needs inthese cases are comparatively simple andwe do not need to enter onto lengthy orcomplicated negotiations and no writtencontract is normally executed.。
德尔厘38SQ说明书
A TRUE DEHLER –SPEED MEETS QUALITY_ SINCE 1963, Dehler has been developing sailing yachts that epitomise performance cruising and the power of innovation. This continuous quest for excellence has resulted in yet another leap forward. It is a yacht that carries the founding principles inits very name: the Dehler 38SQ.DETAILS MAKE THE DIFFERENCE_ State of the art performance cruiser. With smartnew developments, the Dehler 38SQ scores in all areas: comfort, quality and performance. For an enhancedsailing experience from the first to the last moment.Additional windows in the coach-roof bring in lots of natural light.Retractable footrests , flush-mounted into the cockpit sole, allow an especially comfortable footing on the heel.The fixed bowsprit with built-in anchor arm puts the tack point for a gennaker or Dehler Freeride even further forward.Choose high-performance squaretop sails to increaseefficiency and reduce heel.The yacht’s sharp, distinctive lines reflect her progressive design and impressive dynamics.STIRRING PERFORMANCE TURBO CHARGED _ Take on the sporting challenge. Give your Dehler 38SQ that extra bit of dynamism and trim the yacht for maximum sailing performance. Select carbon rigging, squaretop membrane sails, extended bowsprit and racing winches.EFFORTLESS CRUISING. LAID-BACK MOOD._Let the sea breeze carry you. The wind and the Dehler 38SQ do all the work for you. Sheets and halyards run directly to the helm, putting everything within reach. Sail handling becomes truly relaxing.LAP OF LUXURY_Once you have reached your anchorage, the Dehler 38SQ will continue to inspire you.The cockpit offers plenty of space to relax – and the perfect atmosphere at any time.The full teak decking is enhanced with an all-round LED light strip for ambient lighting.WATCH EXTERIORGALLERY HERE_ Let your soul take a holiday. The bathing platform with handrail andflush-mounted bathing ladder is the perfect place for it. Celebrate the end of an unforgettable day on the large, comfortable cockpit benches.SUPREME COMFORT.FLAWLESSLY FINISHED._ A cockpit for sailing enthusiasts. Everything is just so: from sports steering wheels with Y-spokes to the flush-mounted traveller. The entire cockpit is on a single level, with free access to the bathing platform. The cockpit coaming flows smoothly into the rounded instrument consoles, which noticeably lengthen the benches.EVERY LINE WORKS IN HARMONY_Magnetic attraction from every angle. Cleaner lines. A sportier look. More striking hull windows - and a bowsprit perfectly integrated into the deckline. The newly designed coachroof now offers an extra saloon window on each side.CLASS TAKES MANY FORMS. HERE ARE THREE.STANDARD MAST HEIGHT ABOVE WL 17.70m / 58'1"MAINSAIL 43.00m 2 / 463sq ft HULL LOA 12.07m / 39'7"Hull length 11.30m / 37'1"LWL 10.40m / 34'1"Beam 3.75m / 12'4DRAUGHT Standard 2.03m / 6'8"Competition 2.24m / 7'5"Shallow 1.60m / 5'3"DISPLACEMENT Standard 7.50t / 16,534lbs Competition 7.00t / 15,432lbs Shallow 7.60t / 16,755lbs BALLAST Standard 2.38t / 5,247lbs Competition 2.05t / 4,508lbs Shallow 2.75t / 6,062lbs ENGINE Diesel 29PS / hp TANKS Fresh water 295l / 77.93gal Fuel tank 160l / 42.27gal HULL DESIGN judel / vrolijk & co CE CERTIFICATE A - 6 / B - 10SPINNAKER competition 101.70m 2 / 1,095sq ft GENNAKER standard 103.70m 2 / 1,116sq ft competition 121.00m 2 / 1,302sq ft DEHLER 82.10m 2 / 884sq ftCOMPETITION CARBON MAST HEIGHT ABOVE WL 17.80m / 58’5“COMPETITION ALU MAST HEIGHT ABOVE WL 17.70m / 58’1“MAINSAIL DOWNLOAD SPECIFICATIONSHERE21AN AMBIENCE SHAPED BY ELEGANCE_ A homage to light. Brightness characterises the noble interior of the Dehler 38SQ. Every surface contributes to the friendly, sunny atmosphere. One design element in particular is lavishly exploited: natural light. Noticeably larger windows in the saloon and cabins make you forget you are below deck.WATCH INTERIOR GALLERYHERE23 22SUPERB FABRICSNATURALLY ILLUMINATED_Coherent interior design. Off-white walls perfectly match any upholsteryfabric. Handrails in black add an effective highlight. The double-leafsaloon table connects both sofas – or, when folded, leaves the way to theforward cabin free.The first-class collectionof upholstery has beencarefully matched to theinterior design.2524Fine furniture woods are used extensively. Each variation features its special, characteristic grain.TIME FOR GREAT CUISINE_ Enjoyment with all the trimmings. A refrigerator with top and side access, a pull-out wine rack in the saloon table: the living area is full of smart details. There is enough storage space for all your crew’s culinary desires.27PURE LUXURY BATHED IN LIGHT_ Exquisite fittings. Larger hull windows bring natural light into the owner’s cabin. Clever indirect lighting adds the finishing touches. The large designer bathroom with separate shower area also owes its charm to this use of light.28CABIN LAYOUT| STANDARD| OPTION DECK LAYOUT| OPTIONLarge master cabinA1B1Bathroom,L-pantry andlong sofa1 large doubleberth cabinand 1 largestorage roomC1Large mastercabin with islanddouble berthA2Bathroom,L-pantry andsofa with fixedchart tableB2C22 large doubleberth cabinsLarge mastercabin with islanddouble berthA2Bathroom,L-pantry andsofa with slidablechart tableB32 large doubleberth cabinsC2Dehleruni doorconceptDehleruni doorconceptDehleruni doorconceptLAYOUT FORYOUR LIFESTYLE_Tailored to your lifestyle.saloon, an island bed for the owners or a second cabinaft for your guests: your way of life decides.DOWNLOAD CABINCONCEPTS HERE321.EXTRA HIGH GUARDRAILfor maximum safety at the helm.2.FULL SANDWICH HULLBalsa wood sandwich core laminated with premium quality vinylester resin –rigid and lightweight.3. COMPOSITE BULKHEADThe shower compartment is designed as a separate bulkhead. It integrates seamlessly into the hull design and is particularly easy to clean.4.SMARTLY PLACED PUMPTo reduce noise, the freshwater pump is installed outside the cabins.5. K EEL STEPPED MASTfor optimal distribution of forces, more stability, better trim.6. B OW THRUSTERfolds out when needed.7. EXTRA STRONG CHAINPLATES Reinforced with ten layers of glass fibre, the chainplates can withstand enormous tensile forces.8. D EHLER CARBON CAGEThe floor structure is reinforced with carbon fibre at key stress points.Torsion in the hull is minimised under high rig loads and in high seas,enab-ling it to better withstand the forces of water and wind.9. H OT-AIR HEATING SYSTEMDiesel-operated, programmable.1. E XTRA HIGH GUARDRAIL2.FULL SANDWICH HULLPOSITE BULKHEADADVANCED ENGINEERING. IN EVERY DETAIL.4.SMARTLY PLACED PUMP5.KEEL STEPPED MAST6.BOW THRUSTERFRESHWATER TANK295 litresBATTERIES90Ah starter, 160Ah service7.EXTRA STRONG CHAINPLATES8.DEHLER CARBON CAGE9.HOT AIR HEATING SYSTEMENGINE 29HP / 21kWFUEL TANK 160 litres3534| Durable, UV protective gray taffeta | Ultralight film (layers 2 & 4)| H igh-tenacity carbon and aramid fibre and filament matrix UNPARALLED MEMBRANE CONSTRUCTION| Durable, UV protective gray taffeta | Ultralight film (layers 2 & 5)| 60° High-tenacity polyester | 0° High-tenacity polyester QUALITY CRAFTSMANSHIP Every panel is precision cut and hand assembled.PROTECTIVE LAYER Taffeta skins layer each panel for added durability and shape retention.LOW-STRETCHCOMPOSITE PANELS Carefully mappedstretch-resistant polyester composite panels for optimal performance.POWERFUL SAILS FOR PASSIONATE SAILORS_ Fueled by the best sailors, sailmakers and designers in the world and comprehensive data and insights from every project they’ve worked on – from superyachts to dinghies – Quantum developed their latest high-tech products for Dehler yachts.The result is a custom sail engineered to achieve the perfect shapes that, simply put, give you confidence through control and ease of use for the best experience on the water time and time again.DEHLER FREERIDE | 62.80M 2UV-PROTECTEDINTEGRATED TORSION CABLE AND ENDLESS is the perfect intermediate size between genoa and gennaker, offering the largest wind range in its class. That means, the FREERIDE speeds up your Dehler, no matter if you are sailing a close reach or broad reach course. Fully optimised for single-handed sailing, it is set out of the specially designed sailbag at deck level. Attaching it to the anchor bracket and gennaker halyard takes two simple clicks. The rolled-up sail can remain set as second forestay in the marina. It is operated with the gennaker sheets using any winch in37dark grey T 7156dark blue RAL 5004palma blue M 5922 (metallic)off white T 9130oyster white T 9128 flag blue T 5153GELCOAT HULL,WATERLINE & COVELINE PAINTED HULL,WATERLINE & COVELINEsunfast red T 3150off white T 91303938EXTERIOR | COVERS & UPHOLSTERY_ Top-quality fabrics defy any weather and shape the appearance of your Dehler with contemporary maritime colors.EXTERIOR |NATURAL TEAK & SYNTHETIC TEAKMAINDROP, SPRAYHOOD, STEERING WHEEL COVER, COCKPIT TABLE COVER OPTIONSdark grey light grey creamblack light grey dark grey dark blue beige weathered look | white caulking weathered look | black caulking teakNATURAL TEAK OPTIONCOCKPIT CUSHIONS OPTIONSscrubbed look | black caulking scrubbed look | grey caulking scrubbed look | white caulking teak look | black caulkingteak look | grey caulking teak look | white caulking SYNTHETIC TEAK OPTIONS41OPTIONINTERIOR | SURFACESFURNITURE WOOD STANDARDmahoganyteakoak dark grey OPTIONSclassic stripesaustralian acacia FLOORBOARDS STANDARDnoce neroOPTIONSWORKTOP GALLEY STANDARDmuscat / silver piping oyster / black piping cliffside / blue piping graphite / gold pipingFINEST MATERIALS TO SUIT YOUR TASTEINTERIOR | UPHOLSTERY Mix and match as you wish. All interior upholstery can be matched with the following piping colours: gold, silver, red, blue and black.PACIFIC OPTIONSADRIATIC LEATHER OPTIONSmud / black piping ivory / blue piping clay / red piping basalt / gold pipingINTERIOR | UPHOLSTERYstone / silver piping silver / red piping ARCTIC OPTIONStaupe / blue piping denim / gold piping BALTIC STANDARDcream / gold piping43High-end sound meets high-class livingYour first impression: brilliance. Even the finest acoustic nuances are brought out. Two pairs of loudspeakers – one in the cockpit, one in the saloon – overwhelm your ears with their outstanding clarity. Simplicity is the second thing you’ll notice. We’ve brought the design and operation of the system back to the essentials, for intuitive control via the chart plotter or the separate control head. And thirdly, you’ll enjoy the thrill of cutting-edge technology. The system is wireless, very compact and almost limitlessly flexible. This is the connectivity of the future.RemoteJL Audio MMR-40Audio Head Unit JL Audio MM 50 BEwith bluetoothControl via B&G Zeus³ 7“ chartplotterSpeakers 2 x 2 JL AudiospeakersJL Entertainment Package:DEHLER CONNECT – BE SMART, BE INTELLIGENT AND UP TO DATEThe MyDehler Safety Cloud enables real-time monitoring of your Dehler: anytime, anywhere, simply via the app. Protect your precious yacht remotely, as if you lived on board. You can organise maintenance and service with unprecedented ease. Thanks to the electronic logbook, a smartphone is all you need to share your sailing experiences with others. In short: this system will add a whole new dimension to your sailing passion.*MyDehler Safety CloudAlertsNotifications for battery, bilge, shore power, anchor, geo fencing and more.Report IssueDirect contact to the dealer.SensorsReal-time monitoring of battery levels and devices.Switch ControlControl of lighting and electrical devices (optional).TripsElectronic logbook with archive and share function for social media platforms.InsuranceExclusive in-app offers and conclusion of all insurances around the boat by Pantaenius.MaintenancePush notifications before due dates for maintenance of all components.Shop & PartsFeature for ordering equipment, supplies and spare parts.Manuals and operating instructions for all units and components on board.* The range of functions depends on the selected equipment. Please ask your dealer.MyDehler Sound Theatre424544CRUISINGCRUISING PACKAGEI Teak on coach roof, cockpit bottom and bathing platform I Bathing platform, manual fold-out with swimming ladder I 2 additional cleats, midship, retractable (1 each side)I A nchor windlass, electrical with automatic fuse, remote control with chain counterI Delta-anchor 16kg, galvanised with 30m galvanised chain I 2 vents for coach roof hatches I M yDehler Safety Cloud with 24 months subscription and device installed on boardI Battery set, capacity: 1x 90Ah + 2x 160Ah AGM I Blind set with flyscreens for hatchesI Blinds for hull windows and side coach roof windows I Wind indicator I FlagpoleI 6 fenders, 4 mooring lines, plaited I Dehler maintenance kitUPGRADE I FLEXITEEK (colour selection)I F lexiteek on coach roof, cockpit bottom, cockpit benches and bathing platformUPGRADE I STAINLESS STEEL ANCHOR WITH CHAIN I D elta-anchor 16kg, stainless steel, with ‘Power Ball’ swivel and 50m stainless steel chain I Upgrade – Battery set Lithium-ionI Battery set, capacity: 1x 90Ah + 3x 105Ah Li-ion batteriesCOMPETITIONCOMPETITION PACKAGE I Cove line – Competition I Rudder – Competition I 2 LEWMAR 45 Race Plus manual halyard winches I 2 LEWMAR 50 Race Plus manual secondary winches I 2 LEWMAR 50 Race Plus manual mainsheet winches I G enoa tracks (Competition), ball bearing sliders, adjustable from cockpitI Jib barber hauler with low-friction ring I Spinlock removable throttleUPGRADE | ELECTRIC HALYARD WINCH I 2 LEWMAR 45 Race halyard winches, port: manual – stb: electric with automatic fuse UPGRADE | COMPETITION KEEL I T -keel, cast iron/lead, (Competition) draught: 2.24mENTERTAINMENTJL ENTERTAINMENT PACKAGE I J L Audio MediaMaster 50 with bluetooth – for saloon and cockpit I 2x 2 JL Audio speakers in saloon and cockpitI JL Audio MMR-40 remote controlGENNAKERGENNAKER PACKAGEI QUANTUM Gennaker (colour selection)I Squeezer for Gennaker I G ennaker/Freeride package incl. halyard, 2 sheets, 2 blocks and padeyes UPGRADE I COMPETITION GENNAKER I C ompetition composite bowsprit with integrated anchor fitting I Q UANTUM Competition Gennaker (colour selection)Market availability and production capacity may vary. Consult the price list or contact your dealer for specific information.REFINE YOUR DEHLER WITH THE BEST_ Top quality equipment packages for your Dehler 38SQ. You will find full details of each component in the price list. Or contact your Dehler dealer.NAVIGATIONB&G NAVIGATION PACKAGE | CRUISING I Instrument pod on helm station stb I 2 B&G Triton² multifunction displays, 1 per helm station, incl. transducer (wind/depth/speed/temperature)I B &G VHF V60 at chart table, incl. wireless remote handset H60I B&G Zeus³ 7“ chartplotter, stb helm station I B &G Autopilot with Triton² control unit and Precision 9 compass I V HF preparation with antenna and splitter for FM and AISUPGRADE I COMPETITION I 2 B&G H5000 multifunction displays, 1 per helm station, incl. transducer(depth/speed/temperature) and wind sensor at vertical carbon mast head unit I B &G Autopilot with H5000 control unit and Precision 9 compass I B &G CPU Hydra computer(only with B&G H5000 instrument)UPGRADE I SECOND CHARTPLOTTER I Instrument pod on helm station psI B&G Zeus³ 7“ chartplotter, ps helm stationhave been delivered by Dehler since 1963 –an experience that results in excellence.932 INNOVATIONSthat made sailing and living on board significantlymore enjoyable were invented by Dehler.65 MODELSin all sizes up to 60 feet were createdby our designers and developers.58 YEARSof yacht building have continuously increasedthe demands we place on ourselves and made usone of the leading sailing boat manufacturers.1 PROMISEfollows from all that we’ve achieved so far:To build our next Dehler 38SQ exactly as you desire it.47Dehler Yachts UKChandlery Building, Hamble Point Marina, Hamble, Southampton SO31 4NBDesign: www.smz.de | Print: Eggers Druckerei & Verlag GmbH | Photos: Nico Krauss, HanseYachts AG. This brochure is not contractual. The yachts depicted partly comprise special equipment not included in the standard scope of supply. Illustrations may not correspond with current versions. Subject to alterations in design and equipment without notice and errors excepted.©2021 Dehler I CIBD38SQ/A/0321。
beam 公式
Attractors of a rotating viscoelastic beam
M. Abolghasemia , M.A. Jalalib ; ∗
b Institute a Aerospace
Assume an element of the beam at the distance x = r + x from the axis of rotation. The components of the velocity vector for the chosen element are expressed by ˙ + w sin p; vx = u vy = (r + x + u) cos p − wp; ˙ vz = w ˙ − (r + x + u) sin p; (1)
0020-7462/03/$ - see front matter ? 2002 Elsevier Science Ltd. All rights reserved. PII: S 0 0 2 0 - 7 4 6 2 ( 0 1 ) 0 0 1 3 0 - 5
740
M. Abolghasemi, M.A. Jalali / International Journal of Non-Linear Mechanics 38 (2003) 739 – 751
angle. We consider non-linear strain–displacement relations and take further steps towards the understanding of spatio-temporal chaos and attractors. In Section 2, we ÿnd the governing equations of motion using Hamilton’s principle. In Section 3, we introduce proper eigenfunctions that specify the approximate shape of the deformed beam versus the spatial coordinate x, which is measured in the longitudinal direction. Using a new perturbative approach in Section 4, we determine the asymptotic solutions of the governing equations by reducing partial di erential equations to ordinary ones using Galerkin’s projection. We express the zeroth- and ÿrst-order solutions in terms of a small parameter (dimensionless damping coe cient) for elastic and viscoelastic media, respectively. We also show that stable limit-cycles do exist for the system under investigation both in the absence and in the presence of structural damping. We conÿrm our results with the predictions of Liouville’s theorem. 2. Equations of motion Consider a rotating beam as shown in Fig. 1. is the angular velocity of the main shaft and r is the radius of the hub. The de ection of the beam is negligible in the y-direction because of the high area moment about the z -axis. Hence, we investigate the longitudinal and transversal displacements in the directions of x and z , respectively. We deÿne the pitch angle p(t ) as the rotation of the beam about the x-axis. The variable p(t ) is adjusted with the aim of preventing helicopter blades from stalling during the retrieving motion [7].
基于动态超表面天线的雷达通信一体化设计
doi:10.3969/j.issn.1003-3114.2023.05.021引用格式:高克,张海洋,王保云.基于动态超表面天线的雷达通信一体化设计[J].无线电通信技术,2023,49(5):946-952.[GAO Ke,ZHANG Haiyang,WANG Baoyun.Beamforming Design for Dual-functional Radar-communication Systems with Dynamic Metasurface Antennas[J].Radio Communications Technology,2023,49(5):946-952.]基于动态超表面天线的雷达通信一体化设计高㊀克,张海洋,王保云(南京邮电大学通信与信息工程学院,江苏南京210003)摘㊀要:雷达通信一体化(Dual-Functional Radar-Communication,DFRC)利用相同的硬件平台㊁频谱资源同时实现雷达感知和无线通信双功能,是当前无线通信领域研究的热点技术㊂针对动态超表面天线(Dynamic Metasurface Antenna,DMA)辅助的雷达通信一体化系统,研究了最优波束成形设计问题㊂最优波束成形设计是一个非凸优化问题,很难直接求解㊂设计全数字天线架构下的最优波束,将动态超表面天线雷达波束设计转换为拟合最优编码矩阵问题㊂转换后的波束设计问题仍为非凸,为此将其分解为两个子问题交替最小化,其中两个子问题分别采用黎曼共轭梯度和半正定松弛算法求解㊂数值仿真表明,满足通信质量约束的情况下,动态超表面天线架构的DFRC 雷达波束性能接近于无频谱共享时的纯雷达波束性能㊂关键词:雷达通信一体化;动态超表面天线;交替最小化;黎曼共轭梯度;半正定松弛中图分类号:TN929.5㊀㊀㊀文献标志码:A㊀㊀㊀开放科学(资源服务)标识码(OSID):文章编号:1003-3114(2023)05-0946-07Beamforming Design for Dual-functional Radar-communicationSystems with Dynamic Metasurface AntennasGAO Ke,ZHANG Haiyang,WANG Baoyun(Communication and Information Engineering,Nanjing University of Posts and Telecommunications,Nanjing 210003,China)Abstract :Dual-Functional Radar-Communication (DFRC)uses same hardware platform and spectrum re-sources to realize dualfunctions of radar detection and wireless communication simultaneously,which is a hot topic in the field of wireless communications.Forthe Dynamic Metasurface Antennas (DMA)-assisted DFRC system,an optimal beamforming design problem is studied.The optimalbeamforming design is a non-convex optimization problem that is difficult to solve directly.In this paper,an optimal beam with a digitalantenna architecture is designed first,and then the dynamic metamaterial antenna radar beam design is converted into a fitting optimalcoding matrix problem.Though the resulting design problem is still non-convex.it can be decom-posed into two sub-problems and then been solved alternately.In particular,the two sub-problems are solved by riemannian conjugate gradient and semidefinite relaxation algo-rithms,respectively.Finally,numerical results show that the performance of our proposed beamforming design for DMA-assisted DFRC system is close to that of the radar only beamforming without communication requirement.Keywords :DFRC;DMA;alternate minimization;riemannian conjugate gradient;semidefinite relaxation收稿日期:2023-05-050 引言随着5G 时代的到来,无线设备数量和种类均呈现出了爆发性增长,全球通信产业对无线频谱的需求日益迫切㊂有很多场景需要感知与通信联合设计,例如:自动驾驶㊁智慧城市和智能家居等[1]㊂与此同时,随着无线通信速率需求的不断提高,载波频率被推向了传统上分配给雷达系统的毫米波频率频段[2]㊂未来后5G 及6G 时代,为提高频谱效率以及降低雷达与通信系统之间的电磁干扰问题,雷达通信一体化(Dual-Functional Radar-Communication,DFRC)系统成为了一个有前途的热门研究领域㊂在雷达通信一体化系统中,雷达与通信系统之间共享相同的硬件平台和频谱资源,同时实现通信和雷达感知的双功能㊂在雷达通信一体化系统中,由于雷达和通信具有不同的需求且共享相同的资源,因此需要精心设计传输波束以平衡二者的性能㊂为了在保证通信用户服务质量的同时提高雷达的性能,文献[3]研究了发射波束成形优化设计㊂针对全数字天线架构,文献[4]考虑波束之间的相互干扰因素,设计了性能更优的雷达波束㊂考虑到全数字天线功耗大㊁成本高的问题,目前对雷达通信一体化系统研究比较广泛的是基于相移器的混合波束天线架构[5-10],其中文献[5-6]研究了设计模拟和数字预编码矩阵,使其与最优通信预编码矩阵和最优雷达波束预编码矩阵之间误差的加权总和最小;文献[7-8]研究主要集中在雷达波束与理想波束差距小于一定阈值作为约束条件,最大化用户通信质量;文献[9-10]研究了在保证用户通信质量前提下,最优化雷达波束性能,其雷达的波束性能直接由雷达接收机的信干扰加噪声比(Signal to Interference plus Noise Ratio, SINR)决定㊂智能超表面是当前无线通信领域的另外一个研究热点,其可用于增强无线通信盲区覆盖㊁物理层辅助安全通信㊁大规模D2D(Device-to-Device)通信㊁物联网中无线携能通信以及室内覆盖等领域[11]㊂然而,智能超表面除了用来做被动的反射外,还可以用来实现低功耗的主动收发天线㊂动态超表面天线(Dynamic Metasurface Antennas,DMA)是一种典型的基于超表面天线的收发天线㊂在基于DMA的收发器中,每个超表面天线单元是由低功耗的超表面组成,且每个天线单元的幅频特性可以动态实时调控[12]㊂DMA天线架构可以被视为混合模拟数字天线架构,即它不需要额外的专用模拟相移器网络,仅利用自身的信号处理功能便可实现模拟预编码[13]㊂此外,DMA可以包含大量可调谐的超表面天线元件,并且其天线单元之间的距离可以是亚波长,DMA需要的物理面积可以更小,有助于设备的小型化[14]㊂1㊀系统模型和问题描述1.1㊀系统模型雷达通信一体化系统场景示意图如图1所示,一个雷达通信一体化基站拥有N T根天线,为K个单天线用户提供通信服务并探测区域内目标㊂基站使用的动态超表面天线架构,其由数字预编码矩阵㊁L T条射频链路和模拟预编码矩阵组成㊂图1㊀雷达通信一体化系统场景示意图Fig.1㊀Schematic diagram of DFRC基带信号表示为sɪKˑ1,s i~(0,1),iɪ{1, 2, ,K}为第i个用户接收到的信息符号㊂发射信号可以表示为:y=UF DMA F BB s,(1)式中:F DMAɪN TˑL T为DMA天线模拟预编码矩阵, F BBɪN DMAˑK为数字预编码矩阵,DMA微带内的信号传播公式为:u i,j=e-ρi,j(αi+jβi),∀i,j,其中αi为波导衰减系数,βi为波数,ρi,j表示第i微带中第l个单元的位置,其中U((i-1)L+l,(i-1)L+l)=u i,l,L为每条微带上单元的个数[13]㊂功率约束条件为 UF DMA F BB 2FɤP max,P max为基带最大分配功率㊂F DMA矩阵满足以下形式[15]:F DMA=t10 00t2 0︙︙︙00 t L Téëêêêêêùûúúúúú,(2)式中:t iɪN TN DMAˑ1,非零相q i,l=j+e jφi,l2,{φi,lɪ[0,2π]}ɪF DMA,∀i,l㊂雷达在θ角方向的传输功率波束图可以表示为:P(θ;R)=a H(θ)Ra(θ),(3)式中:RɪN TˑN T为传输波束的协方差矩阵,R= UF DMA F BB ss H F H BB F H DMA U-H=UF DMA F BB F H BB F H DMA U H㊂对于N个天线单元的均匀线性天线阵列,其导向矢量为:a(θ)=1N[1,e j2πλdsin(θ), ,e j2πλd(N-1)sin(θ)]T,(4)式中:λ为信号波长,d=λ/2为天线单元间距㊂雷达在θ1和θ2两角之间的波束互相关可以表示为:P c(θ1,θ2;R)=a H(θ1)Ra T(θ2)㊂(5)由式(3)和式(5)可以看出,雷达的传输功率波束图和波束互相关都是由传输波束的协方差矩阵R决定㊂通过波束方向误差和波束互相关两部分的加权和组成一个损失函数,用损失函数评估雷达性能㊂第一部分可以用接收到的波束与理想波束之间的均方差来评估:L r,1(R,α)=1LðL l=1|αd(θl)-P(θl;R)|2,(6)式中:α为比例因子,d(θl)为θl方向理想接收波束㊂第二部分用波束互相关均方差来评估:L r,2(R)=2P2-PðP-1p=1㊀ðP q=p+1|P c(θ-p,θ-q);R|2㊂(7)㊀㊀将以上两部分加权和后,雷达波束图的损失函数表示为:L r(R,α)=L r,1(R,α)+ωL r,2(R)㊂(8)在本文雷达通信一体化系统中,假设通信用户是单天线的,则第k个用户接收信号为:y k=h H k UF DMA F BB,k s k+ðK iʂk h H k UF DMA F BB,i s i+n k,(9)式中:h kɪN Tˑ1为基站与第k个用户之间的下行通道,n k~(0,σ2k)为第k个用户加性高斯白噪声(Additive White Gaussian Noise,AWGN)㊂第k个用户接收信号的SINR可以表示为:γk=|h H k UF DMA F BB,k|2σ2k+ðK iʂk|h H k UF DMA F BB,i|2㊂(10)1.2㊀问题描述雷达通信一体化系统需要权衡通信和雷达之间的性能㊂基于动态超表面天线的雷达通信一体化系统,在保证每个通信用户的SINR高于给定阈值前提下的式(10),使雷达传输波束的性能达到最优的式(8)㊂另外,加上预编码矩阵有功率限制和模拟预编码矩阵相位限制的式(2),雷达通信一体化系统传输波束成形设计问题可以表示为:㊀min FBB,F DMA L r(R,α)㊀㊀㊀㊀㊀㊀㊀㊀㊀㊀s.t.㊀ UF DMA F BB 2FɤP max,F DMA(i,l)=j+e jφi,l2,φi,lɪ[0,2π],|h H k UF DMA F BB,k|2σ2k+ðK iʂk|h H k UF DMA F BB,i|2ȡΓ,(11)式中:Γ为给定用户的SINR阈值㊂式(11)涉及到数字预编码矩阵和模拟预编码矩阵的联合设计,并且问题本身也是非凸的,很难求解㊂当天线架构为全数字天线架构时,该问题对应的问题容易求解,并且在用户SINR满足一定阈值时,其最优预编码矩阵获得的波束与理想波束十分相似㊂因此可以先求出全数字天线最优预编码矩阵,然后将动态超表面天线的模拟预编码矩阵和数字预编码矩阵拟合全数字天线的最优预编码矩阵,由此得到动态超表面天线的模拟与数字最优预编码矩阵㊂2㊀雷达通信一体化波束成形设计2.1㊀基于全数字天线架构先设计基于全数字天线架构的雷达通信一体化系统预编码矩阵W,使其在满足功率约束和用户SINR高于一定阈值前提下,雷达波束性能达到最优㊂其问题表示为:㊀㊀㊀min R L r(R,α)s.t.㊀R=WW HɪS+MW 2FɤP max|h H k w k|2σ2k+ðK iʂk|h H k w i|2ȡΓ,(12)式中:w i为W的第i列,W=(w1,w2 ,w K)㊂将第三个约束化简后的问题为:min R,RkL r(R,α)s.t.㊀R=WW HɪS+MW 2FɤP maxRkɪS+M,rank(R k)=1,k=1,2, ,K(1-Γ-1)h H k R k h kȡh H k Rh k+σ2k,(13)式中:R k=w k w H k,R=ðK k=1R k㊂由于其中的约束条件rank(R k)=1,k=1,2, , K是非凸的,可以先将其松弛掉,松弛后的问题是凸问题:min R,RkL r(R,α)s.t.㊀R=WW HɪS+MW 2FɤP maxRkɪS+M,k=1,2, ,K(1-Γ-1)h H k R k h kȡh H k Rh k+σ2kW=(w1,w2, ,w K),R k=w k w H k㊂(14)可以用Matlab中CVX工具箱求得最优解:R^, R^k,k=1,2, ,K㊂如果式(14)全局最优解满足R^kɪS+M,k=1,2, ,K 秩为1,那么求解式(13)中使用的松弛就是紧的,即松弛后问题的解也是原非凸问题的解㊂定理1㊀式(13)存在最优解R ~,R ~k ,k =1,2, ,K ,满足rank(R ~k )=1,k =1,2, ,K ㊂证明㊀R ^,R ^i ,i =1,2, ,K 为式(14)的全局最优解,将R ^,R ^i,i =1,2, ,K 做以下变换:R ~=R ^,w ~i =(h H i R ^i h i )-1/2R ^i h i ,R ~i =w ~i w ~H i ,R ~,R ~i ,i =1,2, ,K 为半正定矩阵且秩为一㊂因为R ~=R^,并且式(13)和式(14)的最终问题是相同的,所以R ~是式(13)全局最优解㊂现在只要证明R ~,R ~i ,i =1,2, ,K 为式(13)的可行解,则R ~,R ~i ,i =1,2, ,K 为式(13)的全局最优解㊂由于h H kR ~k h k =h H kw ~k w ~H k h k =h H k R ^k h k ,将其带入到(1-Γ-1)h H k R ~k h k=(1-Γ-1)h H k R ^k h k ȡh H k R ^k h k +σ2k =h H k R ~k h k +σ2k 满足式(13)的限制条件㊂所以R ~,R ~i ,i =1,2, ,K 为原问题的全局最优解㊂由定理1可知将式(14)最优解做以下变换:R ~=R ^,w ~k =(h H k R ^k h k )-1/2R ^k h k ,R ~k=w ~k w ~H k ,R ~k ɪS +M ,k=1,2, ,K 且秩为1,并且R ~仍为原问题的解㊂由此可以求解得到全数字天线最优预编码矩阵的列向量w k ,全数字天线架构的最优预编码矩阵W 也就可以求出㊂2.2㊀基于动态超表面天线架构在上节求解得到了全数字天线最优预编码矩阵,本节设计动态超表面天线架构预编码矩阵,使雷达通信一体化系统在满足功率约束㊁模拟预编码矩阵相位约束和通信用户信干扰加噪声比高于一定阈值前提下,最优拟合全数字天线预编码矩阵,其问题表示为:min F BB ,F DMAUF DMA F BB -W ~2Fs.t.㊀ UF DMA F BB 2F ɤP maxq i ,l =j +ej φi ,l2,φi ,l ɪ[0,2π]}{ɪF DMA ,∀i ,l|h H kUF DMA F BB,k|2σ2k+ðKi ʂk|h H kUF DMA F BB,i|2ȡΓ㊂(15)由于此问题不是凸问题,故将问题分解成设计两个子问题相互迭代来求解,两个子问题分别设计数字和模拟预编码矩阵㊂然而,数字和模拟预编码矩阵的设计问题都是非凸问题㊂为此,本文分别采用半正定松弛(Semidefinite Relaxation,SDR )技术[16-17]和黎曼共轭梯度(Riemannian Conjugate Gra-dient,RCG)算法[18]分别设计最优数字和模拟预编码矩阵㊂2.2.1设计模拟预编码矩阵当固定数字预编码矩阵F BB 设计最优模拟预编码矩阵时,限制条件只有模拟预编码矩阵的相位限制㊂其问题为:min FDMAUF DMA F BB -W ~2Fs.t.㊀q i ,l =j +ej φi ,l2,φi ,l ɪ[0,2π]}{ɪF DMA ,∀i ,l ㊂(16)由于问题是矩阵形式,不方便求解,所以将矩阵向量化:min FDMAUF DMA F BB -W ~2F =min F DMA(F T BB U )vec(F DMA )-w 2F ,式中:w =vec(W ~)㊂因为vec(F DMA )中的元素除了相位限制元素,其他为零元素㊂由于零元素的具体位置是已知的,所以可以先将零元素剔除掉㊂令q 为vec(F DMA )去除零元素后的向量,A 为(F T BB U )去除掉与vec(F DMA )零元素相对应的列向量㊂此时的问题转换为:㊀min F DMA(F T BB U )vec(F DMA )-w 2F =min q(Aq -w )H (Aq -w )=min qq H A H Aq -2q H A H w +w H w ㊂(17)由于模拟预编码矩阵的非零元素q i ,l 可以描述为圆心点为0,12e j π2(),半径为12的复平面圆上:q i ,l -12e j π2=12,定义向量b 为:b k =2q k -e j π2,所以q =12b +e j π21(),|b k |=1㊂最终可以将问题转换为关于向量b 的问题:min bq H A H Aq -2q H A H w +w H w =min b 14b +e j π21()H A H A b +e j π21()-b +e j π21()H A H w +w H w s.t.㊀|b k |=1ɪb ,(18)这时搜索空间为N T 个复数圆上,是一个N T的黎曼子流形,可以通过RCG 求得最优解b opt ㊂其中该问题的黎曼梯度为Δf (bt +1k)=AH㊃12A b t +1k +e j π21()-w ()㊂由于F DMA 非零位置是已知的,所以将最优解bopt扩展成矩阵形式,可以得到最优模拟预编码矩阵F opt DMA ㊂2.2.2设计模拟预编码矩阵当固定模拟预编码矩阵F DMA 时,限制条件为预编码矩阵功率约束和通信SINR 阈值约束,其问题为:㊀㊀㊀㊀min F BBUF DMA F BB -W ~ 2F㊀㊀㊀㊀s.t.㊀ UF DMA F BB 2FɤP maxh H k UF DMA F BB,k2σ2k+ðKi ʂk|h H kUF DMA F BB,i |2ȡΓ㊂(19)由于式(19)中第二个限制条件F BB 是按列展开的,所以将问题中的矩阵F BB 和W ~也按列展开:ðKk =1UF DMA F BB,k-W ~k 2F =ðK k =1F H BB,k F H DMA U H UF DMA F BB,k -2F H BB,k F H DMA U H W ~k +W ~Hk W ~k ㊂(20)展开后的问题并不容易求解,引入辅助变量t 2=1,可以化解成二次约束二次规划问题(Quadrati-cally Constrained Quadratic Programs,QCQP):v -k =F BB,kt(),Q k =F H DMA U H UF DMA ,-F H DMA U HW ~k ㊀㊀-W ~H k UF DMA ,W ~H k W ~k(),F H BB,k F H DMA U H U F DMA F BB,k -2F H BB,k F H DMA U H W ~k +W ~H k W ~k=v -H k Q v -k ㊂但此时,由于式(20)中第二个限制条件是非凸的,所以该问题也是非凸的㊂引用SDR 技术将问题进行化简,令V k =v -k v -H k ,rank(V k )=1,可以将问题简化为SDR 的标准形式:min V k ðKk =1tr(Q k V k )s.t.㊀ðKk =1trF H DMA U HUF DMA ,00,()V k ()ɤP max ,∀k ,trH k ,00,0()V k ()Γ-ðKi ʂktrH k ,00,()V i ()ȡσ2k ,tr0K ∗K ,00,1()V k ()=1,V k ȡ0,rank(V k )=1,H k =F H DMA U H h k h Hk UF DMA ㊂(21)由于约束项rank(V k )=1是非凸的,先将其松弛掉,之后的问题是凸问题,可以用Matlab 中CVX 工具箱求最优解V opt k ㊂如果该问题可解或有界,则ðKk =1[rank(V opt k )]ɤK +1,又因为每个用户的SINR 阈值限制,最优解满足:rank (V opt k )ȡ1,所以其最优解满足rank(V opt k )=1㊂由此证得rank(V k )=1的松弛是紧的,V opt k是原问题的最优解㊂F opt BB,k 是V optk的最大特征向量乘以最大特征值的平方根,因此,可以得到最优数字预编码矩阵F opt BB ㊂3 仿真分析本节采用数值仿真验证DMA 雷达通信一体化设计算法的性能,并且与全数字天线架构㊁基于相移器的混合波束天线架构和理想雷达波束进行对比㊂考虑雷达通信一体化基站的天线为均匀线性天线阵列,总发射功率为1W 和天线数量为24,其为用户提供通信服务并探测区域内目标㊂在探测区域内设置了方向为-40㊁0ʎ和40ʎ的3个理想目标,其波束表达式为:d (θ)=1,θ0-Δ2ɤθɤθ0+Δ20,㊀㊀otherwise{,(22)式中:Δ为理想波束的宽度,设置为2ʎ㊂当系统设计的DMA 射频链路为12个,信噪比设置为20dB 时,不同天线架构随角度变化的波速比较如图2所示㊂不同天线架构在满足用户需求前提下,使雷达波束达到最优的仿真,图中K =0㊁FD㊁DMA 和BP 线分别为理想目标波束㊁全数字天线架构波束㊁DMA 天线架构波束和基于相移器架构波束㊂可以看出,全数字天线的雷达波束图基本与理想的波束重合,DMA 天线架构和基于相移器架构也很好地还原了最优波束图,并且从中很容易查找出在-40ʎ㊁0ʎ和40ʎ方向有目标,因为这3个方向的波束峰值明显高于其他方向㊂图3是在4个通信用户SINR 的阈值从6dB 调整到14dB,不同天线架构随角度变化的波束比较㊂图2与图3对比可知,在通信用户阈值提高的情况下,DMA 架构和基于相移器的混合架构的目标雷达波束图峰值有明显的变差㊂图4是在6个通信用户信SINR 的阈值为6dB 情况下,不同天线架构随角度变化的波束比较㊂图2与图4对比可知,服务通信用户增加,目标雷达波束图峰值会变差㊂图5是在4个通信用户信SINR 的阈值为6dB,功率约束调整为2W 情况下,不同天线架构随角度变化的波束比较㊂图2与图5对比可知,增加发射功率,图5中目标雷达波束图峰值接近图2中目标峰值的2倍㊂图2㊀不同天线架构随角度变化的波束比较Fig.2㊀Comparison of beams varying by angle fordifferent antennaarchitectures图3㊀调整用户SINR 后的波束比较Fig.3㊀Beam comparison after adjusting theuser sSINR图4㊀调整用户个数后的波束比较Fig.4㊀Beam comparison after adjusting the number ofusers图5㊀调整功率约束后的波束比较Fig.5㊀Beam comparison after adjusting power constraints图6展示了基于DMA 的雷达一体化系统在不同发射功率情况下,用户SINR 阈值约束和雷达波束性能之间的权衡㊂可以看出,在发射功率一定时,随着用户SINR 阈值的增加,DMA 天线预编码矩阵与全数字天线预编码矩阵之间的均方差也在增加,并且发射功率为2W 时的均方差明显大于功率为1W 的设计㊂这是因为当通信质量要求增加时,为满足用户质量需要消耗更多的功率,而生成雷达波束的功率会变少,雷达波束性能也会变差㊂因此,降低通信质量要求,可以提高雷达波束性能㊂图6㊀用户SINR 阈值与雷达波束均方差之间关系Fig.6㊀Relationship between the user s SINR threshold andthe mean square deviation of the radarbeam4 结束语本文研究了基于动态超表面天线的雷达通信一体化系统,设计了相应的最优波束成形策略㊂采用了数字预编码矩阵与模拟预编码矩阵设计联合交替优化设计,分别应用半正定松弛和黎曼共轭梯度算法求解㊂数值仿真结果表明,所提算法设计的动态超表面天线架构的雷达通信一体化系统,在满足通信用户性能的前提下,其雷达性能接近理想雷达波束㊂动态超表面天线架构与基于相移器的混合波束天线架构整体性能相似,其雷达通信一体化系统中雷达与通信性能之间存在负相关,雷达性能随着通信性能的提高而降低㊂参考文献[1]㊀刘凡,袁伟杰,原进宏,等.雷达通信频谱共享及一体化:综述与展望[J].雷达学报,2020,10(3):467-484. [2]㊀ZHENG L,LOPS M,ELDAR Y C,et al.Radar and Com-munication Coexistence:An Overview:A Review of RecentMethods[J].IEEE Signal Processing Magazine,2019,36(5):85-99.[3]㊀CHU J,LIU R,LIU Y,et al.AN-aided Secure Beamform-ing Design for Dual-functional Radar-communication Sys-tems[C]ʊ2021IEEE/CIC International Conference onCommunications in China(ICCC Workshops).Xiamen:IEEE,2021:54-59.[4]㊀LIU X,HUANG T,SHLEZINGER N,et al.Joint TransmitBeamforming for Multiuser MIMO Communications andMIMO Radar[J].IEEE Transactions on Signal Process-ing,2020,68:3929-3944.[5]㊀KAUSHIK A,MASOUROS C,LIU F.Hardware EfficientJoint Radar-communications with Hybrid Precoding andRF Chain Optimization[C]ʊICC2021-IEEE InternationalConference on Communications.Montreal:IEEE,2021:1-6.[6]㊀LIU F,MASOUROS C.Hybrid Beamforming with Sub-arrayed MIMO Radar:Enabling Joint Sensing and Commu-nication at mmWave Band[C]ʊICASSP2019-2019IEEE International Conference on Acoustics,Speech andSignal Processing(ICASSP).Brighton:IEEE,2019:7770-7774.[7]㊀CHENG Z,LIAO B,HE Z.Hybrid Transceiver Design forDual-functional Radar-communication System[C]ʊ2020IEEE11th Sensor Array and Multichannel Signal Process-ing Workshop(SAM).Hangzhou:IEEE,2020:1-5. [8]㊀CHENG Z,HE Z,LIAO B.Hybrid Beamforming for Multi-carrier Dual-function Radar-communication System[J].IEEE Transactions on Cognitive Communications and Net-working,2021,7(3):1002-1015.[9]㊀CHEN C Y,VAIDYANATHAN P.MIMO Radar Wave-form Optimization with Prior Information of the ExtendedTarget and Clutter[J].IEEE Transactions on Signal Pro-cessing,2009,57(9):3533-3544.[10]DAI Y,HAN K,WEI G,et al.Hybrid Beamforming forDFRC System Based on SINR Performance Metric[C]ʊ2021IEEE/CIC International Conference on Communicationsin China(ICCC Workshops).Xiamen,IEEE,2021:82-87.[11]LAN G,IMANI M F,DEL HOUGNE P,et al.WirelessSensing Using Dynamic Metasurface Antennas:Challengesand Opportunities[J].IEEE Communications Magazine,2020,58(6):66-71.[12]SMITH D R,YURDUSEVEN O,MANCERA L P,et al.Analysis of a Waveguide-fed Metasurface Antenna[J].Physical Review Applied,2017,8(5):054048. [13]ZHANG H,SHLEZINGER N,GUIDI F,et al.Beam Focu-sing for Near-field Multiuser MIMO Communications[J].IEEE Transactions on Wireless Communications,2022,21(9):7476-7490.[14]SHLEZINGER N,ALEXANDROPOULOS G C,IMANI M F,et al.Dynamic Metasurface Antennas for6G ExtremeMassive MIMO Communications[J].IEEE WirelessCommunications,2021,28(2):106-113. [15]SHLEZINGER N,DICKER O,ELDAR Y C,et al.Dynam-ic Metasurface Antennas for Uplink Massive MIMO Sys-tems[J].IEEE Transactions on Communications,2019,67(10):6829-6843.[16]LUO Z Q,MA W K,SO A M C,et al.Semidefinite Relax-ation of Quadratic Optimization Problems[J].IEEE Sig-nal Processing Magazine,2010,27(3):20-34. [17]ZHANG S.Quadratic Maximization and Semidefinite Re-lax-ation[J].Mathematical Programming,2000,87:453-465.[18]YU X,SHEN J C,ZHANG J,et al.Alternating Minimiza-tion Algorithms for Hybrid Precoding in Millimeter WaveMIMO Systems[J].IEEE Journal of Selected Topics inSignal Processing,2016,10(3):485-500.作者简介:㊀㊀高㊀克㊀男,(1994 ),硕士研究生㊂主要研究方向:雷达通信信号处理㊂张海洋㊀男,(1987 ),博士研究生㊂主要研究方向:无线通信信号处理㊁面向6G近场无线通信㊂王保云㊀男,(1967 ),博士,教授㊂主要研究方向:香农信息论㊁无线通信中的博弈与协作㊁无线通信中的信号处理技术㊁视频信息的分析与理解㊂。
cet6
Unit 3Earth Probe Plan Wo ul d Blast a Path to the CoreA scientist proposes sending a grape fr uit-size communication device into the heart of the Earth by blasting a crack in the surface and pouring in a huge quantity of molten iron. The weight of the liquid m e tal would crack the Earth for more than 1,800 miles (3,000 kilometers), carrying the probe to the planet’s core in about a week.The probe would measure temperature, electrical conductivity, and chemical composition, and w ould beam back data as encoded sound wa v es to a surface detecto r.Am bitious or ModestDavid J. Stevenson of the California In stitute of Technology in Pasadena outlines the plan in the May 16 issue of the scientific journal N ature."Planetary missions have enhanced our understanding of the solar system and how planets work,bu t no comparable exploratory effort has been directed towards the Earth' s interior, where equally fascinating scientific issues are waiting to be in v estigated," Stevenson said in his pape r. "I propose a scheme for a mission to the Earth's core, in which a small communication probe would be conveyed in a huge volume of liquid-iron alloy (合金) migrating down to the core along a crack that is propagating under the action of gravity. "The proposal might sound ambitious, but it' s modest in comparison with the demands of space ex ploration, Stevenson said."We live on the Earth's surface, which di v ides what is above fr om what is below. The part a bove us,the rest of the universe, is mostly emp ty, mostly unknown.…The part below is crammed with interesting stuff and is also mostly unknown, despite its much greater proximity to us. "Stevenson calculated that the energy required to create the crack to launch the probe would be eq uivalent to a few megatons (兆吨) of TNT, an earthquake of magnitude 7 on the Richter scale, or a nuclear device such as those already possessed by many nations.It may also be feasible to make use of existing favorable stress environments in the Earth and to avoid the use of nuclear devices,Stevenson said in his paper. "The technological challenge of initiating the crack should be less than that posed by the 1\Ianhattan Pr oject," he said,referring to the code name for Am erica's first atomic bomb.According to Stevenson's calculations,it should be possible to send a probe all the way to Earth's core by combining several proven technologies with a few well-grounded scientific assumptions about the workings of the plane t.To Kn ow the Inside of the Earth"We've spent more than (U.S.) $10 billion in unmanned missions to the planets," said Stevenson,who is the Van Osdol Professor of Planetary Science at Caltech. "But we've only been down about ten kilometers (6 miles) into our own plane t. "The benefits to science would be significant, Stevenson said, because so little has beendirectly observed about the inner workings of the Earth. Scientists do not know, for example, the exact composition or even the temperature of the core, and what they do know is based on inferences about seismic (与地震相关的) data accumulated during earthquakes.Stevenson said his proposal should be attractive to the scientific community because it is of the same scale, price-wise, as planetary exploratio n. To date, NASA has flown unmanned missions past all the planets except Pluto, has made a few highly successful soft landings on Mars, has probed the clouds of Jupiter, is getting ready to probe the atmosphere of Titan, and has sent four spacecraft into interstellar space. Sending something into the Earth, Stevenson believes, will have comparable payoffs in the quest for knowledge."Wh en we fly to other worlds, we are often surprised by what we find, and I think the same will be the case if we go down."A Million Tons of M olten IronAccording to Stevenson, the crack that will have to be blasted into the Earth's surfac e to launch the probe will need to be several hundred meters in depth, and about a foot (30 centimeters) wide, to accommodate a volume of about 100,000 to several million tons of molten iron.The instant the crack opens, the entire volume of iron will be dropped in, completely filling the open space, he said. Through the sheer force of its weight, the iron will create a continuing crack that will open all the way to the planet's core 3,000 kilometers (1,800 miles) below. Anything on a smaller scale may not work; anything larger will be even more expensive, so Stevenson thinks a crack of those dimensions is about righ t."Once you set that condition up, the crack is self-perpetuating (能使自身永久存在的)," Stevenson said.“It’s fundamentally different fr om drilling, where it gets harder and harder—and eventually futile (无效果的)—the farther you go down."The iron will continue to fall due to gravity because it is about twice the density of the surrounding materia l. Riding along in the mass of liquid iron will be one or more probes made of a material robust enough to withstand the heat and pressure. The probe will perhaps be the size of a grape fr uit but definitely small enough to ride easily inside the 12-inch (30-centimeter) crack without getting wedged, Ste v enson said.In side the probe will be instrumentation for data collection, which will be relayed through low-intens ity mechanical waves of some sort. Because radio waves cannot propagate through Earth, this is the only way to get the data transferred, Stevenson said.Based on the rate the molten iron would fall due to gravity, the ball would move downward into Earth at roughly human running pace (about 10 miles / 16 kilometers per hour)Ste ven son said."Each of the principles involved is based on sound knowledge of crack propagation, fluid dynamics, mechanical-wave propagation, and ‘stress states',’’ Stevenson said. "If these things didn't already work in nature, we would have no volcanoes and poorly performing bathroom plumbing, but little to fear from a pebble shattering our windshields."Biggest QuestionThe biggest question should not be the cost, but whether we should pursue the goal of exploring Earth's interior, he said. "That said, I'd suggest we do it if we can keep the cost under (U.S.) $10 billion."This proposal is modest compared with the space program, Stevenson said,and may seem unrealistic only because so little effort has been devoted to i t. "The time has come for action."1. The Earth probe plan aims to discover the inner structure of our plane t.2. Compared with the demands of space exploration, this plan is quite ambitious.3. The technological challenge of blasting a crack should be 1ess than that of the first atomicbomb.4. The Van Osdol Professor of Planetary Science at Caltech points that although we have touchedthe outer space, we have only been 10 miles into our own plane t.5. Professor Stevenson thinks that we w ould be surprised by what we find ________, justlike how we feel when we fly to other worlds.6. Stevenson thinks a crack that is _______ deep is about right to launch the probe into the Earth.7. As Stevenson says, blasting a crack is more effective than _______ because the farther we godown, the harder it becomes.8. Since_____ cannot propagate through Earth,low-intensity mechanical waves of some sortwill be used to transfer the data.9. Because the molten iron would fall due to gra v ity, the ball would move downward into Earth at_______.10. The biggest question of this plan is w hether we should pursue the goal of ________ but not thecos t.Short-answer Questions:Questions 1 to 5 are based on the following passage.Most Am ericans spend far more of their leisure time with the mass media than in any other occupation. In addition, most of us hear, see, or read some of the media while engaged in other activities. Thus an extremely large number of our waking hours are spent with the mass media. Of all the media, television is clearly dominant, with newspapers a close second, at least as a source of news and other information. Our exposure to all media is important, however, because all of them contribute materials for the construction of that world in our heads. For most people, increased use of one medium does not decrease use of anothe r. In fact, in certain cases, and especially for certain purposes, the more one uses one medium, the more likely one is to use others.There are various factors that can cause you to expose yourself to the media selectively, avoiding much of the material with which you disagree. Some of that selective exposure is probably due to the psychological pressure you feel to avoid the discomfort caused byconfrontation with facts and ideas contrary to your beliefs, attitudes, or behavio r. However, some selective exposure is not due to the pressure for consistency but to other factors, such as your age, education, and even the area in which you live and the people with whom you associate.Quite a different sort of factor that affects your media experiences is the social context of exposure: whether you are alone or with others when you are exposed to a medium; whether you are at home, at the office, in a theater, and so on. These contexts are as much as a potential part of the message you will form as film images on the screen or words on the page. In addition, that social context affects—both directly and indirectly—the media and the media content to which you become exposed. New fr iends or colleagues get you interested in different things. Other members of the family often select media content that you would not have selected, and you become exposed to i t.These various factors have so much influence on your media exposure that so little of that exposure is planned.Questions: (注意:答题尽量简短,超过10个词要扣分,每条横线限写一个英语单词,标点符号不占格。
面向国际化的哈工大计算机学科本科生培养
Passive Lecture
Video Taped Lecture
Study
Team Problem Solving
EXAM
Team LEAD
Before Video Taped Lecture
DTeam Problem Solving
EXAM
12
提
纲
1
学科发展的新趋势、新形势、新任务、新挑战、新机遇
21世纪,重大科学技术创新与计算机学科密切相关
芯片与计算装置
• • • • • • 物理学 化学 生物学 材料科学 信息科学 „„
Nanometer Transistor
Quantum Computer
DNA Computer
5
新趋势
21世纪,重大科学发现越来越呈现 多学科融合态势 人类基因组科学工程(HGP)
Celera Designer
6
新形势
“提高质量是高等教育发展的核心任务”“全面提高高等 教育质量的核心是大力提升人才培养水平”“牢固确立人 才培养在学校各项工作中的中心地位和本科教学在大学教 育中的基础地位”--《教育部、财政部关于“十二五”期 间实施“高等学校本科教学质量与教学改革工程”的意见》 大力提升人才培养水平、增强科学研究能力、服务经济 社会发展。“教育部关于全面提高高等教育质量的若干 意见(教高[2012]4号)”
8
新挑战
普适而言,计算机学科创新人才如何培养?
科学先进的课程体系
扎实系统的理论与专业课程 前沿交叉的科学视野
9
新机遇
MOOCs和移动互联网加速了教育的全球
化,并为课程质量的提高创造了前所未
有的机遇。
SPOC为提高课堂教学质量提供了新的 有效手段
BDS Start to End Simulation说明书
BDS, Start to End Simulation, BDS Start to End Simulation Simulation Codes Summary yD. SchulteD SchultePresentations•Deepa Angal-Kalinin: Beam dynamics issues in BDSg p •Peter Tenenbaum: Possible migration to Accelerator Makeup Language•Glen White: BDS tuning simulation•Andrea Latina:Static and Dynamic Alignment of the CLIC BDS Andrea Latina: Static and Dynamic Alignment of the CLIC BDS •Javier Resta Lopez: Start to End simulations with intra-train feedbackTony Hartin:Luminosity performance with multiple feedbacks •Tony Hartin: Luminosity performance with multiple feedbacks •Peter Tenenbaum: Lucretia status and plans•Andrea Latina: PLACET : New features and plans•Paul Lebrun: CHEF status and plan•Roger Barlow: Issues in Simulating the Effects of Wakefields •Steve Malton: Interfacing BDSIM with PLACET, wakefield Steve Malton:Interfacing BDSIM with PLACET wakefieldcalculations of collimator•Isabell Melzer-Pellmann: Lumi scans with wakefields in MerlinBDS tasks related to LET (1)()•BDS has the most different styles of magnets;BDS has the most different styles of magnets;standardize the magnets and reduce the styles •Magnets on strings–Additional correctors/PSs–How will it affect the tuning + beam basedalignment–How will it affect the performance after push-pull •Temperature requirements in the tunnel and its effect on beam stabilityb bili•Stability requirements for push-pull•Angle feedback and integration of other feedbacks?Angle feedback and integration of other feedbacks?•Effect of wakes from pumping ports, vacuum chamber misalignments, resistive wall, IR wakes, HOM heating, wake fields from crab, spoilers, other transitions….k fi ld f b il th t itiBDS tasks related to LET (2) Laser wire•Define requirements on emittance measurement (absolute/relative) of train (or bunch) every ? second? Æbeam tuning procedureof train(or bunch)every?second?beam tuning procedure •The present design of laser wire assumes 300 scans per train, which drives the requirements of the laserD d b t i di ti b t lli ti•Do we need any beam spotsize diagnostics between collimation region and IP (somewhere in the final focus?)yCrab system–To understand and verify requirements on the crab cavity mode damping from beam dynamics point of view. e.g.g,y 10E+4 for SOM is difficult from RF design, but may berelaxed with intra-train feedback?–The alignment of crab cavity and effects of the orbit offset in sextupoles may be perhaps fixed with some smallin sextupoles may be perhaps fixed with some smallvertical crab cavity nearby the main one.•Low energy parameters•Work plan is being developed•Lattices to be frozen in autumBDS AlignmentBDS Ali t100nm BPM resolution needed in sextupoles•100nm BPM resolution needed in sextupoles•Quad shunting+DFSy p–Is the systematic error important?•Multi-knobs, also high order needed•Studies using one beam and it’s mirror yield 90% at better than 110%l i it110% luminosity–Independent beams yield 90% at better than75%slower convergence–slower convergence•1e-3 magnet error significantly impacts convergence•Intra-pulse beam-beam offset feedback kick limited by sextupole •200nm stability requirement for quadrupoles•Main goal is to have a verification by another studyATF2•ATF2 is an important test•Can take advantage of flight simulators•Need to fully study alignment and tuning Need to fully study alignment and tuning –E.g. losses can be a problem•Simulation of ATF2Simulation of ATF2–Spot size measurement is slow (1 minute)–Convergence speed crucial–Spot size growth 1nm/hourCLIC BDS Alignment •Few-to-few and DFS used•DFS problematic since response to energy deviation not linear•Collimations system alignment works •FFS alone does not workFull optimisation (brute force) with simplex •Full optimisation(brute force)with simplex works on 50% of the casesy–No solution yet•Could still be starting point for ILC second BDS alignment studyg yCLIC BDS Dynamic Effects•Choice of orbit feedback gain–Ground motion requires yields gain>0.01 tocorrect orbit–BPM resolution requires gain<0.3BPM l ti i i03•Very tight quadrupole stability requirements –Fractions of nm for final doublet–Nanometer for other magnets–Need to use stabilisation•Should also run this for ILCI t t d F db k St di Integrated Feedback Studies Continuation of studies started by Glen •Continuation of studies started by Glen•From linac to IP–Including fast IP feedbackIncluding fast IP feedback–Bunch compressor should come soonMulti bunch tracking•Multi-bunch tracking–Realistic main linac, undulator not usedy g y •Ground motion C or K yield 85% of target luminosity •Smoother luminosity increase during feedback than before–Banana effect is less important•Crab cavities and collimator wakefields to be includedFeedback Optimisation •Basic idea is to exploit luminosityinformation to speed up beam-beam i f ti t d b boffset feedback convergence•Based on Javier’s integrated simulation •Luminosity based on pair signal Luminosity based on pair signal•Optimise gain for minimum luminosity loss•Looks an interesting approachBeam-Beam Scans •Translate emittance growth intoluminosity lossTry to optimise collision in presence of •Try to optimise collision in presence of imperfection along the machine •Banana effect is reduced compared to B ff t i d d d t TESLAWakefield Models •Linear wakefields seem OK for main studiest di•Need something better for loss studiesg•Uncertainties still exist–Comparison between formulaeComparison between formulae•Check proper implementationBenchmarking with experiments–Benchmarking with experiments•Experiments are not easyBDSIM-PLACET Interface•BDSIM is a vital code for BDS studies –Halo and background studies–But not aimed at alignment and tuning studies •Geometry information–Currently: Halo tracking in BDSIM, core inPLACET–General lattice information–ImperfectionsDeck Format•Current deck format is based on XSIF –Parser is available and can be added to programs P i il bl d b dd d t•Slow transition to AML is planned–Until 2010 both formats (XSIF+AML) will beU til2010b th f t(XSIF AML)ill bsupportedAML is similar to XML–AML is similar to XML–An AML parser is available and can be used •Can also read and write SIF•Has been tied to PLACET•Plans exist to tie it to SAD, LUCRETIA and MERLINLUCRETIA •MATLAB based toolkit–Performs tracking–Correction and tuning is user supplied •LIAR and DIMAD are no longer supported •Mass production runs using MATLAB compiler •Used for ATF2•To be included–UndulatorU d l t–IR solenoid–Better cavity wakesBetter cavity wakes•Reference documentation availableTutorial to come–Tutorial to come•Way cool with it’s own cultPLACET•tcl/tk and OCTAVE interfacey–Dynamic libraries•AML interface+some more available •Coherent/incoherent synchrotron radiation •Collimator wakes, also from GdfidL •Misalignment, correction and tuning routines are includedi l d d–Can use your own ones, if you like •Preliminary MPI version existsPreliminary MPI version exists•Halo and tail generation module•Some reference manual availableSome reference manual available–Tutorials on the webOnline help–Online help•Used for ATF2CHEF•A libraryA library–Contains tracking–Correction and tuning left to the userp •Wakefields are to be improved •Significant modifications•XSIF interface rewrittenSome concerns about status of AML •Some concerns about status of AMLConclusion•Integrated simulations move forward •Confirmation of BDS alignment is neededg p •Interesting ideas on feedback improvements •Several codes are being developed–Way cool, way hot...Way cool way hot•More work to be done。
(NEW)北京航空航天大学外国语学院211翻译硕士英语[专业硕士]历年考研真题及详解
A. adulterate B. moor C. vaccinate D. sue 【答案】A 【解析】句意:如果你往食物或饮品之类的东西里掺假,例如往里 面兑水,就会降低它们的质量。adulterate掺杂。moor停泊;固定。 vaccinate注射疫苗。sue控告;起诉。
10. The orphanage is just one of her _____ causes. A. phonetic B. philanthropic C. prevalent D. lunatic 【答案】B 【解析】句意:这座孤儿院只是她的慈善事业之一。philanthropic仁 慈的;慈善的。phonetic语音的。prevalent盛行的,流行的。lunatic精神
2010年北京航空航天大学211翻译 硕士英语考研真题及详解
Part Ⅰ. Vocabulary (30 points) Directions: There are 30 incomplete sentences in this part. For each sentence there are four choices marked A, B, C and D. Choose the ONE answer that best completes the sentence. 1. The _____ is used by astrologers to help calculate the influence of the planets on people’s lives. A. zephyr B. zodiac C. zyme D. zest 【答案】B 【解析】句意:天文学家通过占星术中的黄道十二宫来计算星球对 人类生活的影响。zodiac黄道十二宫(用于占星术)。zephyr和风,微 风。zyme酶。zest热情;热心。
应用笔记52416:Thermo Scientific Nicolet iS50 FT-IR 光谱仪
Thermo Scientific Nicolet iS50 FT-IRSpectrometer: Improving Productivity through Compact Automation Application Note 52416 Key WordsAutomation, Far-IR, FT-IR, Full-spectral, Infrared, Mid-IR, Multi-range,Multiple Methods, Near-IR, Workflow OptimizationChallenges Facing Industrial Analytical LabsMany routine QC/QA laboratories can perform materialanalyses with single range, basic Fourier transform-infrared (FT-IR) instrument configurations. However,modern analytical laboratories face increasing workloadsfrom a broad range of sample types with a simultaneousdrive for faster results and more complex samplecharacterization needs. Flexibility to analyze multiplesample types becomes mandatory when rapidly respondingto these different application requests. Such diversityrequires laboratory instruments to be reconfigured forspecific measurements multiple times per day, taking timeaway from other critical activities. This also implies thatlaboratory personnel possess the necessary skills andexperience to make decisions on how best to configure the instrument for a given application. In addition, frequent handling of delicate optics components presents a costly risk for instrument failure. As a result, many industrial laboratories choose to outsource complex analyses. These limitations inevitably slow the laboratory’s ability to respond to urgent business needs.The Thermo Scientific™ Nicolet™ iS™50 FT-IR spectrometer alleviates many of these productivity concerns by automating setup of the FT-IR system for multi-spectral range experiments (>20,000 cm-1 to 80 cm-1) and fori ntegrating techniques like FT-Raman, near-IR and mid/far-IR attenuated total reflectance (ATR) into a single workflow. Intelligent design behind the Nicolet iS50 spectrometer permits unattended, risk-free operation, increasing lab efficiency, sample throughput, and operational consistency between users. This capability is delivered in an economical, compact system (63 cm of linear bench space) enabling any laboratory to employ multiple techniques for their analysis.Flexibility and Value-added ActivitiesWorking labs need analytical flexibility to respond toa variety of situations where answers are critical for decision-making. Examples include deformulating mixtures to build a case for patent infringement, identifying counterfeit materials for product safety alerts, analyzing forensic samples for criminal investigations, performing failure analysis to minimize production run delays, assessing process scale-up options for a new product launch, or troubleshooting customer complaints. Such diversity of applications requires the selection and installation of the correct instrument accessory as well as choosing the optimal source, beamsplitter, detector, optical path, and experimental conditions. Manually changing components and sampling parameters requires skill and may risk exposure of expensive optics to the external environment (i.e., dust, fingerprints or water vapor). In addition, changing these parameters can result in extensive wait times to equilibrate the instrument before the next measurement.These manual reconfigurations provide little added value to the laboratory workflow. Users must plan and set up batch experiments to minimize the number of steps. This creates bottlenecks, limiting access to the full capability of the instrument. As a result, labs are less able to address “emergency situations” without interrupting the batch run and resetting the instrument parameters. For instance, analysis of a polymer with additives requires mid-IR and far-IR plus Raman spectroscopy. This would entail three beamsplitter changes with associated risks in handling expensive components and instrument recovery times between changes.The productivity improvements with the Nicolet iS50 FT-IR spectrometer come from two main sources. First, the internally mounted iS50 ABX Automated Beamsplitter Exchanger uses one-button simplicity (described as a Touch Point) to perform instrument setup and operation, providing a “one touch and done” workflow. The removal of manual handling and exposure of the optics to the environment means instant readiness. Second, the user need no longer care about which optics are installed. As seen in Table 1, the potential for error in manual operations is apparent when the array of possible component combinations is considered. With the Nicolet iS50 spectrometer, however, a user simply presses the Touch Point on the instrument to automate the configuration and ready the instrument for the experiment. For example, pressing the Touch Point on the iS50 NIR module automates the setup without requiring any understanding of which optics are used. What matters is performing NIR analysis – not worrying about choosing the right components. The instrument takes care of this step. Integration of the spectrometer with its modules and components allows the user to expand capabilities, increasing productivity with tools such as:• Up to three detectors (such as near-, mid- and far-IR)• The iS50 Raman sample compartment module• The built-in diamond iS50 ATR sampling station• T he iS50 NIR module with integrating sphere or fiber optics• The iS50 GC-IR module• A sample compartment thermal gravimetric analysis-IR (TGA-IR Interface)Figure 1 describes the analytical power the user can achieve with the iS50 spectrometer to obtain answers needed for time-sensitive decisions. With a single user interaction, the instrument can perform multiple measurements and analyses, resulting in a final report, even when unattended. The Thermo Scientific OMNIC™software provides a user-friendly interface to set up applications quickly and generate spectra for definitive answers. By adding powerful analytical tools like the Thermo Scientific OMNIC Specta™ software with a library of over 30,000 spectra and multi-component searching (or the TQ Analyst™ software for chemometrics), a complete analytical workflow from sampling to results can often be achieved in less than 60 seconds.This paper will demonstrate how the integration and automation of the Nicolet iS50 spectrometer leads to new levels of productivity, while minimizing risk to costly components. Unlike most spectrometers, operating the Nicolet iS50 instrument becomes simpler as modules are added and as more manual steps are removed even when unattended.Experiment Source Beamsplitter Detector AccessoryMid-IR Transmission Thermo Scientific Polaris™KBr KBr-DLaTGS Standard Cells Far-IR Transmission Polaris Solid Substrate Polyethylene DLaTGS Cells w/Far-IR Windows Near-IR Transmission White Light CaF2InGaAs CuvettesMid-IR ATR Polaris KBr Dedicated DLaTGS iS50 ATRFar-IR ATR Polaris Solid Substrate Dedicated DLaTGS iS50 ATRFT-Raman Raman Laser CaF2Raman InGaAs iS50 RamanTable 1: Experiments made possible with the Nicolet iS50 FT-IR SpectrometerFigure 1: Nicolet iS50 analysis workflowAutomated Multi-spectral Analysis:Mid- and Far-IR ATR plus Near-IRMost FT-IR users understand the utility of the mid-IR spectral range for qualitative and quantitative analyses. Less well known, the far-IR region can provide new and unique information. Simply put, as the mass of atoms involved in vibrations increases, the wavenumber decreases.1Thus, for materials like organometallics or metal oxides, the IR absorption shifts below 400 cm-1 and below the range of standard KBr optics. Numerous polymers, sugars, and other large molecules also have far-IR information which may be useful or definitive to the analyst. Traditionally, collecting FT-IR spectra in both the mid-IR and far-IR region entailed significant sample preparation. This included changing hygroscopic optics and multiple detectors, and risking altered system performance from water vapor. The Nicolet iS50 spectrometer enables rapid analysis over the full mid-IR and well into thefar-IR region (4,000 cm-1 to 80 cm-1) when equipped with the iS50 ABX, iS50 ATR, and the correct beamsplitters. The typical, multi-range FT-IR application requires opening the spectrometer to swap beamsplitters. This requires care in handling costly components and exposesthe internal optics to the environment by disrupting purge or desiccation. This activity adds a recovery period tore-equilibrate the instrument before quality data can be collected. These wait times add no value to operations, wasting the analyst’s precious time. Integration and automation on the spectrometer eliminate non-productive wait times, improving efficiency.As an example, Table 2 compares the steps needed to perform a full spectral analysis from far-IR to near-IR between the manual method (Typical) and the Nicolet iS50 method with built-in iS50 ATR and iS50 NIR module. This represents three spectral ranges in one sampling operation, a unique power of the instrument. Most important the built-in iS50 ATR optics and detector permit spectral data collection in both the mid- and far-IR regions. The analysis time decreases from around 30 minutes to less than seven. With the Nicolet iS50 spectrometer, the user is able to load two sampling locations (the built-in ATR and the Integrating Sphere module), start the macro and walk away, while in the manual operation, continuous attention is needed to swap the beamsplitters at the right moments. This seemingly hidden improvement allows unattended operation, permitting productivity through automation. Figure 2 shows just the mid- and far-IR spectra collected from acetylferrocene analyzed using an OMNIC macro-controlled workflow. The additional information from the far-IR spectra is clear – the low end triplet verifies that the iron is sandwiched between the cyclopentadiene rings. The NIR data is not shown, but the entire process required seven minutes, including collection of themid- and far-IR backgrounds. Automation also reduced the total hands-on time of the user (pressing buttons, loading sample) to ≈20 seconds. Figure 2: Mid-IR and far-IR spectra of Acetylferrocene. The far-IR optics permit collection to 1700 cm-1, which may be sufficient (fingerprint and far-IR) for many applications.Time Nicolet iS50 Time Process Step Typical (minutes) with Built-in ATR (minutes) Sample Preparation Grind, Mix 10 None 0 Mid-IR Background Collect BKG 0.5 Collect BKG (2nd)* 1. Mid-IR Collect Load Sample, 2 Load Sample, 1Collect Spectrum Collect SpectrumChange Optics Manual Exchange 0.5 Automated 0.5 Recovery Time Wait for Purge 5–10 No Recovery Time 0 Far-IR Background Collect BKG 0.5 Collect BKG (1st)* 0.5 Far-IR Collect Load Sample, 2 Load Sample, 1Collect Spectrum Collect SpectrumChange Optics (NIR) Manual Exchange 0.5 Automated 0.5 Recovery Time Wait for Purge 5 No Recovery Time 0 Collect Background Collect BKG 0.5 Collect BKG 0.5 Collect Sample Load Sample, 1 Collect SAM 0.5Collect SAMData Analysis (Search) Perform Search 2 Automated Search 0.5 Total Time 29.5–34.5 6.5 Table 2: Far-infrared analysis: Typical versus Nicolet iS50 process* W ith the iS50 ATR present, the far-IR background (BKG) is collected, the iS50 ABX swaps beamsplitters, and themid-IR background is collected in <1.5 minutes. The sample is loaded and the spectra are collected in sequence.All times are approximate.Figure 3: The Thermo Scientific Nicolet iS50 FT-IR spectrometer configured for FT-Raman, near-IR, and mid/far-IR ATR with the automated beamsplitter exchanger.Figure 4: Touch Points on the Nicolet iS50 spectrometer employ one-button switching between modules and the iS50 ABX automates optics set-up Touch Point A – NIR module Touch Point B – Raman moduleTouch Point C – Built-in diamond ATRComponent D – ABX Automated Beamsplitter ExchangerMultiple Techniques and Multi-range Analysis: Enhanced FlexibilityThe Nicolet iS50 spectrometer can be configured with FT-Raman, NIR, and wide-range diamond ATR. Switching between these experiments raises concerns of instrument recovery time (purge), exposure/handling of optics, and potential confusion or user error. The experiments are often seen as independent activities for these reasons. The spectrometer with iS50 ABX simplifies this apparently complex situation to one step – initiation of a macro. The Nicolet iS50 instrument shown in Figure 3 is configured with the iS50 NIR, iS50 Raman, iS50 ATR and the iS50 ABX modules and shows how easy sample loading and analysis can be done.For operating one module at a time, the user need only press the associated Touch Point. Seen more closely in Figure 4, Touch Points make one-button operation effortless when switching between modules (sampling stations) and automating optics exchange. Rather than thinking through the components needed (light source, beamsplitter, optical path and detector) to run anexperiment, the user simply presses the Touch Point to switch from an ATR to an NIR measurement and waits until the instrument indicates that it is ready to begin. This error-free operation is done in 30 seconds.The Nicolet iS50 analytical power in Figure 1 becomes clear when the four data collections – mid-IR and far-IR ATR, NIR, and Raman – are performed in one workflow. Collecting spectra from each of these modules using a conventional manual approach required about 50 minutes, including sample loading, optical changes, time forequilibration, and optimization of the Raman signal. The analyst needed to be present throughout the experiment to perform the beamsplitter changes and collect various backgrounds for each sampling station. At the end of the 50 minutes, four spectra and their analyses were available. Actual data collection took 5 minutes and total hands-on time was 45 minutes, representing inefficient use of the analyst’s time.In contrast, the results shown in Figure 5 emerged from a single OMNIC-macro operation. The macro wasprogrammed to begin by collecting backgrounds for the mid- and far-IR ATR, and then switched to the iS50 Raman module. Next the samples were loaded on the ATR, NIR, and Raman sampling stations. After optimizing the signal using the autofocus feature of the Ramanmodule, the macro was initiated, and the analyst walked away. From starting the macro to completion of the final report, the analysis took less than 12 minutes, representing a time savings of over 70%. The actual data collection time was again 5 minutes, however, total hands-on time for the analyst was only 2 minutes – a highly efficient use of the analyst’s (and the instrument’s) time.ABC DApplication Note 52416AN52416_E 12/12MAfrica +27 11 822 4120Australia +61 3 9757 4300Austria +43 1 333 50 34 0Belgium +32 53 73 42 41Canada +1 800 530 8447China +86 10 8419 3588Denmark +45 70 23 62 60Europe-Other +43 1 333 50 34 0Finland/Norway/Sweden +46 8 556 468 00France +33 1 60 92 48 00Germany +49 6103 408 1014India +91 22 6742 9434Italy +39 02 950 591Japan +81 45 453 9100Latin America +1 561 688 8700Middle East +43 1 333 50 34 0Netherlands +31 76 579 55 55New Zealand +64 9 980 6700Russia/CIS +43 1 333 50 34 0Spain +34 914 845 965Switzerland +41 61 716 77 00UK +44 1442 233555USA +1 800 532 4752©2012 Thermo Fisher Scientific Inc. All rights reserved. All trademarks are the property of Thermo Fisher Scientific Inc. and its subsidiaries.This information is presented as an example of the capabilities of Thermo Fisher Scientific Inc. products. It is not intended to encourage use of these products in any manners that might infringe the intellectual property rights of others. Specifications, terms and pricing are subject to change. Not all products are available in all countries. Please consult your local sales representative for details.ConclusionMany forces contribute to new pressures on industrial analytical laboratories: increased sample loads, decreased staffing, retirement of experts, and shrinking budgets. The Thermo Scientific Nicolet iS50 FT-IR spectrometer makes a significant contribution to alleviating these challenges through automation in a multi-tasking, single platform instrument. The Nicolet iS50 spectrometer greatly simplifies and streamlines workflows by decreasing the number of steps with one-button ease and macro operations performed by the analyst. In addition, risks inherent in manual operations (e.g., user error, environmentalexposure) and long recovery times are eliminated. Analysts of any skill level can successfully obtain meaningful results with minimal hands-on time.Technology designed to improve workflow can be found in the iS50 ABX and task-specific modules (i.e., Raman, NIR, TGA-IR etc.). The Touch Point operation simplifies access to the full range of capabilities by automatically configuring the optics (near-, mid- and far-IR) andswitching between sampling stations (modules) in secondsfor enhanced productivity. For the modern industrial lab, the Nicolet iS50 FT-IR spectrometer offers a powerful new tool that goes beyond routine FT-IR to more comprehensive analyses (e.g., FT-Raman and far-IR), adding value to laboratory activities in a compact, easy-to-operate platform.References1. H eavy atoms or groups of atoms shift the IR wavenumber value lower, according to the relationshipwhere ˜v is the IR wavenumber (cm -1) and μ is the reduced mass. As the mass (μ) increases, the IR peak shifts to lower wavenumbers.GlossaryCaF 2– calcium fluorideDLaTGS – d euterated L-alanine doped triglycene sulphate InGaAs – Indium gallium arsenide KBr– potassium bromideFigure 5: Multi-technique data for a recyclable plastic component using the spectrometer pictured in Figure 3. Inset shows NIRindependently for clarity.。
gt-power教程-cranktrain
Highlights:Expert-system cranktrain toolbox (piston, conrod, web, etc. ) for easy layout of any (I, V, W) cranktrainRigid, torsional and3D-bending analysis modesRigid kinematics, forces, torques, bearing loads Engine unbalanced forces moments, balance shafts3-D Block vibrations and mounting system analysis Crankshaft torsional vibrations (time and frequency domain)Viscous, rubber dampers, vibration isolators Crankshaft 3D bending: dynamic or quasi-static, crankshaft durabilityMain and conrod bearings analysis (orbits, MOFT, flow, temperature, friction) Predictive friction models for bearings, rings, pistonCranktrain Design AnalysisCranktrain Dynamics, Balance, Mounts and Bearings GT-SUITE performstorsional dynamic analysis of cranktrains in both time and frequencydomains. This analysis mode is used to model torsional vibrations of the crankshaft to recover maximum torsional displacements, strains, stresses etc. and to identify and eliminate any unwanted resonances. Dynamometer couplers, viscous and elastomer dampers, vibra-tion isolators and accessory drives can be accounted for.GT-SUITE offers a complete range of methods and models for the analysis of cranktrain systems and crankshafts in order to address balance, vibration, friction/lubrication, integrity and durability issues, to study the effect of operating parameters and design tradeoffs.GT-SUITE cranktrain models are constructed using elements of a cranktrain toolbox with many ease-of-use features and “expert system” intelligence which automates building of a consistent model. The same model can be used for rigid, torsional or 3D-bending analysis.AdvancedFeatures and Applications:Elastomer damper model based on Maxwell solid approach:consistent treatments in both time and freq. domainsAutomatic extraction of equivalent beam compli-ances of crankwebs (for 3D bending) from 3D FEA static results3D stress, fatigue and crankshaft reliability analysis using 3D FEAunit-load stress recombinationSteady-state or transient simulations, start-stop6 ODE integrators including implicit schemes suitable for stiff bending dynamics. Fast runtimes.Seamless integration in GT-SUITE, with:• Timing drive (e.g. chain)• Valvetrain• Engine performance (GT-POWER)• Oil circuit /Lube system • Vehicle drivetrain (engine recoil, mounts) • Models, to account for system interactionsThese capabilities are included in everyGT-SUITE license applied during pre-processing, to extract properties of an equivalent beam-based model. Models of main and conrod bearings are integrated with cranktrain dynamics in the rigid, torsional or 3D-bending analysis modes. Mixed lubrication of oil films is modeled. Predictions include loads, orbits, MOFT and oil film extent, oil flow and temperature, friction torque and power loss. Bearing models can also be easily linked to a full lubrication circuit model.GT-SUITE integrated model of cranktrain, engine mounting system, and driveline vehicle dynamics is used to investigate driveability/comfort issues.。
Development of Piezoelectric Bending Actuators with Embedded Sensors for Micromech Flapping Mech
Development of Piezoelectric Bending Actuators with Embedded Piezoelectric Sensors for Micromechanical Flapping Mechanisms∗Domenico Campolo,Ranjana Sahai,Ronald S.Fearing{minmo,rsahai,ronf}@Department of EECS,University of California,Berkeley,AAbstractThis paper presents the fabrication and the testing of piezoelectric unimorph actuators with embedded piezo-electric sensors which are meant to be used for the ac-tuation of the Micromechanical Flying Insect(MFI). First the fabrication process of a piezoelectric bending actuator comprising a standard unimorph and a rigid extension is described together with the advantages of adding such an extension.Then the convenience of obtaining an embedded piezoelectric sensor by a sim-ple and inexpensive variation of the fabrication pro-cess is pointed out.A model for the sensor embedded into a unimorph actuator with rigid extension is de-rived together with itsflat response band limits.Cal-ibration steps are also outlined which allow,despite residual parasitic actuator-sensor coupling,the use of the actuator with the embedded sensor for measuring position and inertial forces when external mechanical structures are driven.An experiment is carried out which validates the model for the actuator/sensor de-vice under desired operating conditions.Preliminary application of the fabricated device to the MFI is also presented where the mechanical power fed into the wing is estimated.1IntroductionPiezoelectric actuators are widely used in smart struc-ture applications due to their high bandwidth,high output force,compact size,and high power density properties.For such reasons they are very appeal-ing for mobile microrobotic applications such as the Micromechanical Flying Insect(MFI)[1]where,be-cause of strict size/weight constraints,smart struc-tures capable of both actuating and sensing are pre-ferred.Since the technology needed to fabricate PZT based bending actuators was already available[4],the ∗This work was funded by ONR MURI N00014-98-1-0671, DARPA.possibility of integrating sensorial capabilities into the actuators themselves was investigated.Many works exist where piezoelectric thin patches are bonded to structures in order to sense the deformation of a spe-cific area[2]but,in most of the cases,the process for fabricating unimorph actuators needs to be heav-ily modified.The idea of extending the capabilities of a standard unimorph actuator with a lateral sen-sor came from[6]although no hint was given for the fabrication involved.The possibility of having the sensing section and the actuating section coexisting on the same piezoelectric layer,differentiated by simply patterning the electrode instead of aligning and bonding two different piezo-electric layers next to one another,was investigated. The sensor obtained in this way was affected by a strong electromechanical coupling between the actu-ating area and the sensing area,mainly a parasitic capacitance between the two electrodes.In order to shield such a capacitance,a third grounded electrode was then introduced in between the two sections.2FabricationSince the publication of[4],several improvements have been made to the fabrication of PZT based unimorph actuators.The only parameter unchanged is the ra-tio of thicknesses of the two layers constituting the unimorph since its choice was based upon the output energy optimization criteria[4].The basic unimorph is obtained by bonding together stainless steel and PZT(PZT-5H,T105-H4E-602ce-ramic single sheet,Piezo Systems,Inc.)respectively with thicknesses t s=76.2µm and t p=127µm.Fab-rication details can be found in[4].A different commercial piezoelectric material(PZN-PT from TRS Ceramics,Inc.)will be eventually used for the actuation of the MFI because of its superior properties[4].PZN-PT is a single crystal piezoelec-act sFigure1:Piezoelectric actuator diagram comprising basic unimorph actuator and rigid extension.tric material which is available infixed dimensions. Difficulties arising in reshaping its size,without dam-aging its single crystal properties,impose the use of its original dimensions.On the contrary,PZT is a ce-ramic material,relatively inexpensive,which can be simply reshaped by laser cutting without perceptible loss of its properties.Although much larger,for test-ing purposes,an equivalent unimorph can be made out of PZT which provides,from the mechanical out-put,the same stiffness and blocking force theoreti-cally provided by a PZN-PT based unimorph.Planar dimensions for the PZT based unimorph have been determined to be(width)W act=6mm and(length) L act=12mm.2.1Rigid ExtensionMFI[4]is a biomimetic project and a major design constraint is the wing beat resonance,determined to be at about150Hz.The stiffness of the actuator is therefore designed[4]to resonate,together with wing inertia reflected through an amplifying mech-anism(4-bar mechanism),at this frequency.With the givenfixed dimensions for the PZN-PT based uni-morph,which translate into W act,L act,t s and t p for the PZT based equivalent one,the resulting stiffness would be too large.A rigid extension can be designed so that,by acting as a lever,it would provide larger free displacement at its tip together with lower block-ing force,thus,leading to lower stiffness.In order to obtain the required stiffness,a rigid extension of length L ext=8mm is needed.Rigidity of such an extension is a necessity.Aflexible one would bend, storing part of the actuation energy instead of trans-mitting it to the wing.Afirst idea would be extending the very stainless steel layer which constitutes the uni-morph but it can be easily seen that it would be even more compliant than the unimorph itself.A stiffer structure can be bonded on top of the extended stain-less steel such as a hollow triangular beam as shown in Fig.1.Such a folded structure is much stiffer than a planar structure.It can in fact be made out of thinner, therefore lighter,stainless steel(12.5µm)and still be considered rigid.The lighter the extension the more ideal it can be considered.As shown later,the inertia of the reflected wing is about190mg while the iner-tia of the extension is less than10mg.The dynamics, i.e.the inertial terms,of the extension can then be neglected.Advantages of adding a light and hollow rigid exten-sion instead of having a longer unimorph with similar output mechanical behavior,i.e.stiffness and blocking force at the tip,can be summarized as:−thefinal actuator will be lighter since a hollow beam replaces a comparably long section of the unimorph itself.−higherfirst mode resonant frequency since also the equivalent mass of the actuator,which to-gether with its stiffness defines thefirst resonance, is lighter.−behaving as a lever,the rigid extension represents afirst stage where the actuator tip displacement is pre-amplified.A pre-amplifying stage helps re-ducing nonlinearities deriving from a single high ratio amplifying stage(often needed in piezoelec-tric actuators based applications).−higher energy density can be achieved since the extension converts a force load at the tip into a combination of the same force plus a torque(see Fig.5)at the unimorph tip.Such a combination produces more bending throughout the unimorph than only the force would.2.2Side SensorAs qualitatively described in[6],considering an actu-ator of width W act and length L act constituted by a piezoelectric layer bonded onto an elastic layer,an-other narrow piezoelectric strip of width W s W act and same length as the actuator can be bonded onto the elastic layer,side by side with the piezoelectric layer constituting the unimorph actuator itself.This way it will be subject to the same deflection as the actuator and via the piezoelectric effect a measure of the mean curvature of the actuator can be derived,as shown later.active areaclampGNDFigure2:A photo the piezoelectric layer after laser cutting and top electrode patterning.The sensor should be much narrower than the actua-tor in order not to affect the deflection.Ideally there should be no coupling between the piezoelectric layer of the unimorph and the sensing strip.PZT ceramics can be easily shaped by laser cutting. A532nm(green)laser beam can be generated by the QuikLaze micro-machining system(New Wave Re-search Inc.)which,at its maximum output power,is capable of cutting through PZT quickly enough not to overheat the sample.This allows precisely cutting out the piezoelectric pieces that will be lately bonded onto the stainless steel layer.By reducing the power of the laser beam,it is also possible to pattern the very thin layer of nickel that constitutes the electrod-ing layer of the piezoelectric sheets.Since laser cutting the PZT pieces is a necessary step in the fabrication of the actuator,adding electrode patterning to the cur-rent process is a very inexpensive operation since no alignment has to be done and it takes relatively little time compared with the laser cutting itself.Fig.2shows a photo of the piezoelectric layer whose top side electrode has been patterned with low power laser beam and then cut through with high power laser beam.Its whole length is divided into an active area which will be free to bend together with the elastic layer and the remaining area which,together with the elastic layer,will be clamped and kept from bending. The clamping area is where the wires will contact the electrodes,V pzt for the actuator and V sens for the sen-sor.The presence of a third electrode(GND)is ex-plained below.Differently from previous work[2],in order to keep the fabrication process simple and inexpensive,the actuator and the sensor coexist on the same piece of piezoelectric material.They only differ from one an-other because of the discontinuity of the electrodes,Figure4:Coordinate system:the unimorph actua-tor is a long,narrow and uniform beam along the x axis.Non uniformity,i.e.different materials,is only assumed along the zdirection.of(9)can be substituted into the second leading to: D=d31Y E p S+( T−Y E p d231)E(10) As in[5]and[7],the strain is directly related to the neutral axis z n(x)by:S=−(z−z n)∂2z n(x)∂x2(11)Integrating(10)along z from one electrode located at z1=z p−t p/2to the other located at z2=z p+t p/2and considering that E dz=0when extended between the two grounded electrodes z1and z2:z2z1D dz=d31Y E p z2z1S dz=−∂2z n(x)∂x2d31Y E p z2z1(z−z n)dz(12) Since divergence of the dielectric displacement must be null and only the z-axis component D is here con-sidered,D=constant.Both integrals in(12)can now be evaluated,leading to:D=−d31Y E p(z p−z n)∂2z n(x)∂x2(13)At each point x,the dielectric displacement D is pro-portional to the curvature∂2z n(x)∂x2which is the onlyterm in(13)which varies along x.As in[5],in order to derive the dielectric charge built in the piezoelectric material,theflux of D across the area of one of the electrodes(i.e.Σ=[0W s]×[0L act])can be evaluated as:Q= ΣD dxdy=−W s d31Y E p(z p−z n)∂z n(x)∂x L act0=−W s d31Y E p(z p−z n)αact(14)since the sensor is subjected to the same clamping con-ditions of the actuator,i.e.cantilevered,and therefore∂z n(0)∂x =0and∂z n(L act)∂x=αact.5Model LimitsEquation(14)relates the polarization charge built in the sensor directly to the slopeαtip at the end of uni-morph actuator and before the extension.A simple way to measure the polarization charge is by read-ing the voltage that develops across the sensor elec-trodes when these are left disconnected.In reality piezoelectric materials are affected by several kind of losses,among these the dielectric ones.Considering the piezoelectric layer as a capacitor,if a static charge is initially placed across its electrodes,the capacitor will eventually discharge because of ohmic losses of the dielectric material constituting the capacitor itself.A piezoelectric layer can then be thought of as a pure ca-pacitor C0with a resistance R0in parallel which takes into account the dielectric losses.Elementary circuit theory shows that such a configuration adds a zero in the origin and a pole,i.e.s/(R0C0s+1),to thefi-nal frequency response of the sensor.R0C0represents the discharging time constant of the lossy piezoelectric capacitor.The pole at(R0C0)−1is the lower limit for the fre-quency range at which the sensor provides aflat re-sponse.It is not possible to eliminate the zero in the origin,i.e.the sensor cannot be used at DC or in quasi-static conditions,but it is possible to keep the pole at low frequencies by using a charge amplifier, as shown in Fig. 3.This well known circuit pumps an external charge into the sensing electrode in order to neutralize the polarization charge and to keep the voltage across the piezoelectric layer at zero(virtual ground).In this way,since the voltage is virtually zero,there is no effect due to the dielectric losses.In fact,a charge amplifier as the one in Fig.3beside the capacitor C has to include a resistor R(not shown in the picture)in parallel.Thus instead of being limited by the(R0C0)−1the band is limited by(RC)−1which is controllable and can be set to be small enough not to interfere with the frequency range of interest.5.1Band upper limitTheflat-response band upper limit of the actua-tor/sensor system is solely given by thefirst mode of the unimorph actuator.Such a frequency depends upon the geometrical dimensions of the actuator it-self which should be designed so that thefirst reso-nant mode occurs much after the working bandwidth (100−200Hz for the MFI).Having aflat response simply means that,at any frequency within theflat range,a static model for the actuator is sufficient,i.e. matrices S act and G act are frequency independent. After thefirst resonance,a non-flat response of the unimorph actuator could be theoretically considered andδtip and F tip could still be derived by(7)but G act would now be frequency dependent.6CalibrationCalibration is a necessary step in order to be able to practically use the actuator/sensor device.Both ac-F tip V pztδtip0150V450µm31.3mN0200µmTable1:DC measurement for characterizing the stiff-ness and the free displacement of the actuator. tuator and sensor calibrations need to be performed but while the former can be done at DC,i.e.with a static procedure,the latter has to be done at AC,i.e. dynamically,since the sensor provides no response at DC.As also described in[4],by means of an optical mi-croscope,a digital video camera and a TV screen,it is possible to measure linear deflections ranging in the order of10−103µm.For the actuator,described by (6),only EI and M V(M pzt=M V V pzt)need to be determined since L act and L ext are known.A bending actuator can be characterized at DC by its stiffness and its free displacement.For the former,zero volt-age is applied at the electrodes while for the latter no force is applied at the tip.Table1reports typical values where F tip=31.3mN is applied by hanging a 3g mass at the tip of the actuator.Measurements in Table1are sufficient to calibrate EI and M V from(6) and(8).Calibration for the sensor has to be performed at AC, i.e.dynamically,within theflat response band.With reference to Fig.3,given an(AC)input voltage of am-plitude˜V pzt,a signal of amplitude˜V out can be detected from the charge amplifier and,via optical microscope, the corresponding displacement amplitudes˜δtip and ˜δactcan be measured.The last two measurements are necessary to infer,via(8),˜αact=˜δtip−˜δactext.Frequencyresponse H(jω)=V out(jω)V pzt(jω)of the unloaded actuatorcan be measured by means of a Dynamic Signal Ana-lyzer(HP3562A).For a given general input V pzt(jω), in the frequency domain,αact(jω)can be evaluated as:αact(jω)=−˜αact˜Vout V out(jω)=−˜αact˜Vout H(jω)V pzt(jω)(15)Equation(15)is justified by the fact thatαact is re-lated to the polarization charge Q(and therefore to the voltage V out)by a linear relationship as in(14). Such a multiplying factor is derived by the calibra-tion constants˜αact and˜V out.The minus sign takes into account the inverting functionality of the charge amplifier in Fig.3.Once V pzt is known andαact is derived by(15),δact and F tip can be determined from(7)whileδtip is de-rived from(8).As previously mentioned,the ground shield in Fig.1 is designed to limit the direct coupling between actu-ator and sensor.Although greatly attenuated(actua-tors without such ground shield are affected by a very strong feed-through),it is not completely zeroed,re-sulting in a small offset signal always in phase1with V pzt.Although not perceptible for quantities such as αact,δact andδtip,it is evident for F tip since,when no loading effect is applied at the tip,a non zero force F tip=F0is measured from(7).In order to counterbalance such an offset,(7)can be rewritten as:[δact F tip]T=G act[αact(1+∆off)V pzt]T(16) where G act is now calibrated(since EI and M V are calibrated)and the constant value∆off is used to introduce a counterbalancing offset always in phase with V pzt.∆off is chosen in order to zero(or better minimize)F tip at low frequencies(but still within the flat response frequency range),i.e.canceling out the force offset F0.7Testing and ApplicationAn actuator with an embedded sensor was fabricated as previously described.Its purpose is to be used for driving and sensing,via a4-bar mechanism(basically a lever),a wing attached at the end of the4-bar itself as in Fig.7.Since nonlinear behaviors are expected when dealing with large angular displacements of the wing(due to the4-bar mechanism),the fabricated actuator/sensor device wasfirst tested by means of simple point wise mass m tip=190mg attached at the tip of the ex-tension.A point wise mass was chosen in order to match the inertia of the wing as seen before the4-bar structure,i.e.mimicking the real structure without introducing nonlinearities.The frequency response of such a system was obtained by sweeping,over the fre-quency range of interest for the MFI,a driving signal V pzt of constant amplitude10V peak-to-peak and by 1Since the circuit in Fig.3is meant to measure a charge,any parasitic capacitance C par between the actuating electrode and the sensing one will generate a charge Q par=C par∆V,where ∆V is the voltage between the two electrodes.Because of the operational amplifier,the sensing electrode is kept at virtual ground,i.e.∆V=V pzt.Q par is then proportional to V pzt and therefore always in phase with it.ratio.In particular,a softening of the transformed ac-tuator occurs,i.e.for larger displacement the actuator becomes more compliant.It can be shown,[3],that a damped mass-spring system with a softening spring leads to frequency shift as the ones shown in Fig.8. 8Summary and Future WorkBy patterning the electrodes of a piezoelectric layer by means of a low power laser beam,sensing capabili-ties were embedded into a standard piezoelectric uni-morph actuator.In order to reduce the electromechan-ical coupling between actuating and sensing section an additional electrode was patterned and grounded pro-viding a shielding effect that significantly reduced the coupling.A model was derived for the sensor which, together with the static model of the actuator,pro-vided a simple means of estimating external force and displacement at the tip of the actuator itself.The cal-ibration steps were outlined in order to practically use a fabricated device.A point wise mass was attached at the tip of the actuator and its weight was chosen in order to reproduce the operating conditions arising when an wing is driven,through a coupling mecha-nism,by the actuator.The force measured by the sensor matched the expected ones which were com-puted by perfectly knowing the nature of the load,i.e. the point wise mass.The actuator/sensor device was then used to drive a MFI thorax and the sensor signal was processed to derive the mechanical power fed into the wing,an important information for wingflapping mechanisms.As future work,the actuator/sensor de-vice will be used to induce the wing to track the de-sired kinematics.AcknowledgmentsThe authors would like to thank Srinath Avadhanula, Gabe Moy,Metin Sitti,Joe Yan and Robert J.Wood for useful discussions and assistance. References[1]R.S.Fearing,K.H.Chiang,M.Dickinson, D.L.Pick,M.Sitti,and J.Yan,“Wing Transmission for a Micromechanical Flying Insect,”Proc.of the IEEE Robotics and Automation Conf.,pp.1509-1515,San Francisco,CA,USA,April2000. [2]C.K.Lee,“Piezoelectric Laminates:Theory andExperiments for Distributed Sensors and Actua-tors,”Intelligent Structural Systems,Kluwer Aca-demic Publishers,pp.75-167,December1992. [3]S.Sastry,Nonlinear Systems:Analysis,Stability,and Control,Springer-Verlag,New York,1999.[4]M.Sitti,D.Campolo,J.Yan,R.S.Fearing,T.Su,D.Taylor,and T.Sands,“Development of PZTand PZN-PT Based Unimorph Actuators for Mi-cromechanical Flapping Mechanisms,”IEEE Int.Conf.Robotics and Automation,pp.3839-3846, Seoul Korea,May21-26,2001.[5]J.G.Smits and A.Ballato,“Dynamics Ad-mittance Matrix of Piezoelectric Cantilever Bi-morphs,”Journal of Microelectromechanical Sys-tems,pp.105-112,vol.3,1994.[6]Kenji Uchino,Piezoelectric Actuators and Ul-trasonic Motors,Kluwer Academic Publishers, Boston,1997.[7]M.Weinberg,“Working equations for piezoelectricactuators and sensors,”Journal of Microelectrome-chanical Systems,vol.8,pp.529-533,Dec.1999.。
瑞雷激光振镜说明书
7 MAINTENANCE............................................................................................................21
8 TROUBLESHOOTING..................................................................................................22
5 INSTALLATION ............................................................................................................17
6 6.1 6.2 6.2.utter
The deflection unit is designed to deflect an input laser beam and output it again. The deflection unit cannot block or weaken the laser beam. To prevent unwanted emission of the laser beam, above a particular danger class the laser device must be fitted with a shutter (Ö on page 5, Classification of laser devices). The laser device must be of sufficient quality that the laser beam can only be emitted at the beam output on the deflection unit.
- 1、下载文档前请自行甄别文档内容的完整性,平台不提供额外的编辑、内容补充、找答案等附加服务。
- 2、"仅部分预览"的文档,不可在线预览部分如存在完整性等问题,可反馈申请退款(可完整预览的文档不适用该条件!)。
- 3、如文档侵犯您的权益,请联系客服反馈,我们会尽快为您处理(人工客服工作时间:9:00-18:30)。
Beam Dynamics Issues in an Extended Relativistic Klystron*G. Giordano†, H. Li, N. Goffeney, E. Henestroza, A. Sessler, S. Yu, Lawrence Berkeley Laboratory,Berkeley, CA 94720, T. Houck and G. Westenskow, Lawrence Livermore National Laboratory,Livermore, CA 94550 USAPreliminary studies of beam dynamics in a relativisticklystron were done to support a design study for a 1 TeVrelativistic klystron two-beam accelerator (RK-TBA),11.424 GHz microwave power source. This paper updatesthose studies. An induction accelerator beam is modulated,accelerated to 10 MeV, and injected into the RK with a rfcurrent of about 1.2 kA. The main portion of the RK is the300-m long extraction section comprised of 150 traveling-wave output structures and 900 induction accelerator cells.A periodic system of permanent quadrupole magnets isused for focusing. One and two dimensional numericalstudies of beam modulation, injection into the main RK,transport and longitudinal equilibrium are presented.Transverse beam instability studies including Landaudamping and the “Betatron Node Scheme” are presented.I. BACKGROUNDA preliminary design report (PDR) by a joint LBL-LLNL team investigated an rf power source for the NLClinear collider. [1] This design promises to be competitiveboth in cost and total efficiency with systems based onconventional klystrons using pulse compression. However,it will be necessary to transport the modulated inductionbeam through a 300-m relativistic klystron to achieve thehigh efficiency. Thus, an important part of the PDR studieswas simulating the motion of the beam. Two codesdeveloped at LLNL were used for these simulations: RKS2Code [2] is a 2-1/2 D PIC code with a coupled cavitycircuit model used to simulate the interaction of the beamwith the operating field, TM01 mode, while OMICE [3] is aslice code with a coupled cavity circuit model used tosimulate the transverse dynamics of the beam interactingwith a dominant dipole mode.II. LONGITUDINAL DYNAMICS The longitudinally dynamics that is acceptable for anextended RK can be achieved in the following way:(1) In the main RK section the rf output cavities areinductively detuned (i.e. the phase velocity, v ph, of the 3-celltraveling-wave structures (TWSs) is made faster than the ____________________________________________________________________ *The work was performed under the auspices of the U.S..Department of Energy by Lawrence Berkeley Laboratory under contract AC03-76SF00098 and Lawrence Livermore National Laboratory under contract W-7405-ENG-48.†Visiting scholar from the University of Milano, Italy.1501005012024036048Cavity #Power(MW)Figure 1. Power extraction from 150-cavities in an extended RK: (a) with inductive detuning (v ph= 1.33c);(b) no detuning (v ph= 1.0c).velocity of the particles) to counter the debunching effects caused by space-charge and rf-induced energy spread. In this scheme the particle bunch lags behind the decelerating crest of the wave, with the particles at the bunch tail losing the least energy. Kinematics lead to a 'catching up' mechanism and subsequent synchrotron oscillation in stable rf buckets. The RKS simulations show stable propagation through 150 cavities (Figure 1). For comparison, cavities with no inductive detuning are shown to result in particle debunching after a few cavities.(2) Before the main RK there is a chopper section and an 'adiabatic capture' section, which serve to modulate an initial DC beam into a train of tight bunches. These have the desired properties for beam transport and power extraction in the main RK. The chopper, based on the original Choppertron [4], should generate cleanly separated microbunches at 11.4 GHz with the length of the bunches equivalent to about 240o in longitudinal phase space. In the 'adiabatic capture' region, the microbunch lengths are further reduced by a number of (highly inductive) idler cavities, to 70o[1] which is the desired bunch length for the main RK. In addition to microbunch sharpening, this section also serves to provide the energy transition from 2.5 to 10 MeV [1] with the beam continuously accelerated by the induction machine between the bunching cavities.(3) At the end of the RK is an 'afterburner' section which is to increase overall system efficiency by extracting more power out of the still bunched beam that exits the main RK (without reaccelerating it). The spacing and the impedances of the extraction cavities in this section are varied to compensate the continuous decline of the average energy of the beam as well as changes in the rf bucket.III. TRANSVERSE DYNAMICSThe primary issue for transverse dynamics is beam breakup (BBU) caused by the excitation of higher order modes in beam line structures. The PDR identified two components as sources of BBU. The first is the 900induction cells in the RK with a trapped resonant mode near 4 GHz. A highly damped, conventional cell design described in the PDR has a transverse impedance less than 4 k Ω/m. This value is acceptably low, with Landau damping from the predicted energy spread, to avoid BBU.The output structures are a greater difficulty. The “Betatron Node Scheme,” that relies on the RK’s strong periodic quadrupole focusing, is used to suppress BBU.The technique is described in the following example: A monoenergetic beam describes a betatron oscillation under the influence of a periodic focusing system. Passing through a series of thin cavities, the transverse position of individual electrons is unchanged. However, the transverse momentum increases by ∆p x = Rx , where R is an integral operator. The position and momentum from the exit of one cavity to the next is related through the following matrix transformation.x p x n = 10R 1 cos θ1ωβsin θ-ωβ sin θcos θ x p x n-1.(1)The first matrix represents the momentum change, and the second describes the betatron motion. If the phase advance,θ, is 2π between all cavities, the position and momentum at the n th cavity can be related to the initial conditions:x p x n = 10R 1nx p x 0= 10nR 1x p x 0.(2)Equation (2) indicates that the growth in the transverse momentum, and, therefore, the maximum displacement,increases linearly with the number of cavities. For θ not equal to an integral multiple of π, the growth can be exponential with the number of cavities [5]. While our design has a periodic structure, strong ppm focusing, and a ± % Variat ion from E av eR e l a t i v e G r o w t h a f t e r 300 m2.52.01.51.00.50.0Figure 2. Simulation showing the effect of E ave variation.The insert shows the E ave profile over the pulse.constant average beam energy, there will be energy spread,variation in average energy, errors in the focusing system,and extended cavities. Numerical studies were performed to determine tolerances for realistic conditions. Using reasonable design parameters [6], errors of ± 1.5 % in the magnetic focusing and/or average energy are acceptable. In Fig. 2 the result of one of these studies is shown.IV. RADIAL DEFOCUSING2D numerical simulations carried out with the RKS2code have shown that when the phase velocity, v ph , of the operating mode (TM 01) in a TWS extraction cavity is different from the speed of light (detuned cavity) the beam experiences a radial kick from the field much larger than the case when v ph is equal to c (non-detuned cavity). The radial kick is significantly larger than what is predicted by the Panofsky-Wenzel (P-W) theorem [7] for a closed cavity. The radial kick, if true and uncompensated, will cause the loss of the beam as it traverses the extended RK,as shown in Figure 3. Preliminary analytical and numerical studies have been performed inorder to identify and understand the source(s) of the above discrepency. Two questions need to be answered: (1) How reliable the simulation results are; and (2) How good the resonant cavity model, which the RKS2 code is based upon is in describing the radial focusing force.In developing the analytical model, we assumed a single dominant traveling-wave mode (TM 01) in a cylindrically symmetric cavity. Then, using the impedance of the mode, it can be shown that the radial force acting on an electron traveling in a cavity is (e/2γ2)E r for a non-detuned cavity and e(1–v ph /c)E r for a detuned cavity (where E r is the radial electric field and γ is the relativistic factor). This indicates immediately that the radial force increases by two order of magnitude when the cavity is detuned as compared to the synchronism case (In our present RK design, γ = 20.6 and |1-v ph /c| ≈ 0.3).The corresponding radial momentum change of the particle can be calculated in a first order approximation by integrating the force over the length of the cavity, assuming that the electron's trajectory in the cavity is not affected by the field. For the case where v ph ≠ c the formula is given as the following∆p x =x ⋅–φ2–φ2–ωt o (3)where φ is the phase advance of the wave field per cell, ξ is the amplitude of the electric field on axis, x is the transverse position of the electron with respect to the axis and ω t o is the phase of the electron at the entrance of the cavity with respect to the field.2.01.51.00.50.00.0030.0040.0050.0060.0070.008z ( m )B e a m e n v e l o p e ( m )Figure 3 Beam envelopes in a 2-m reacceleration section after inductively detuned and non-detuned cavities.From eq. (3) we can see that the increase of the radial momentum of the electron due to the wave field has the following features: i) a sinusoidal dependence on the detuning of the cavity (measured by v ph and φ); ii) a sinusoidal dependence on the longitudinal position of the electron in the bunch ωt o ; iii) a linear increase with the distance of the particle from the axis.The above observations agree with the numerical results from RKS2 to within 10% (as shown in Figure 4).The resonant cavity model the RKS2 code based on has been used rather successfully for power balance for TM 01 and BBU study for a dominant dipole mode.However, the validity of the model for the radial focusing force of the field has never been tested.V. CONCLUSIONSWe have demonstrated in 1-D numerical studies the modulation and transport of the induction beam through the RK. Approximately 360 MW of rf (11.424 GHz) power was generated in each of 150 output structures.Longitudinal stability was accomplished by detuning the traveling-wave output structures to compensate for space charge effects and energy spread. Transverse stability required damping of higher order modes in resonant structures, Landau damping, and the “Betatron Node Scheme.”2-D numerical studies are required to study issues related to beam emittance, transverse space charge, and radial focusing. Initial 2-D studies show that the beam experiences a large radial momentum change during transit of the detuned output structures, which does not agree with the P-W theorem. Additional analytical and numerical studies tend to suggest that the discrepency could be caused by the less rigorous treatment in the RKS2 code of the boundary condition that affect the transverse dynamics. So,the effect might not be as serious as the code predict. But,4.54.03.53.02.52.0-60.0-40.0-20.00.020.0(v x /v z )/(x /g a m m a )ω to Figure 4. Normalized transverse phase space vs. phase after one inductively detuned cavity (v ph = 1.33c), analytical and numerical results.if it is, there are available several compensating schemes which can be explored:1) Use exterior cavities that are coupled to the detuned TWSs to compensate the radial defocusing;2) Use non-detuned TWSs as extraction cavities with the longitudinal bunching being provided by idler cavities positioned before and after each of the TWS.VI. REFERENCES[1] S. Yu, et al., "RK-TBA Based Power Source for a 1TeV NLC," LBID-2085/UCRL-ID-119906.(Feb 1995).[2] R. Ryne and S. Yu, Proceedings of 1990 LINAC,pp. 177 and 190 (1990).[3] T. Houck, et al., Proccedings of 1992 LINAC, p.495 (1992).[4] J. Haimson and B. Mecklenburg, "Design and Construction of a Chopper Driven 11.4GHz Traveling Wave RF Generator,” Proceedings of 1989 IEEE-PAC Conf., pp. 243 (1989).[5] V. Neil, et al., Part. Acc. 9, 213 (1979).[6] E. Henestroza, et al., “Design of Inductively Detuned RF Extraction Cavities for the Relativistic Klystron Two-Beam Accelerator,” this conference.[7] W. K. H. Panofsky and W. A. Wenzel, Rev. Sci.Instr., 967 (1956).。