网络资源检索第三次作业

1、1、检索课题名称：重大装备中的动力学、振动与控制问题2、课题分析：中文关键词: 1.动力学 2.振动 3.控制 4.重大装备英文关键词: （1）. Dynamics（2）. Vibration （3）. Control（4）important equipment3、选择检索工具：外文电子期刊4、构建检索策略：Dynamics * Vibration *Control* important equipment 5、简述检索过程:选择快速检索，输入检索词：第一、Dynamics；第二、Vibration；第三、Control;第四、important equipment 检索结果1070

2、6 篇6、根据检索结果选择 3 条记录根据检索结果，浏览题录可以确定该文献的收藏单位（图书馆或情报所、信息中心等），从而 可以进一步确定是否索取或借阅、复制原文。Search Results：10706 records in Compendex for 2000-20121. Uncertainty modeling of structural dynamics for robust vibration controlWang, Feng (Computational Aerodynamics Institute, China Aerodynamics

3、Research and Development Center, Mianyang 621000, China); Li, Dao-Kui; Lei, Yong-Jun Source: Zhendong yu Chongji/Journal of Vibration and Shock, v 28, n 10, p 126-131, October 2009 Language: ChineseDatabase: Compendex Abstract  -  Detailed2. Stewart

4、platform vibration control strategy based on dynamicsYang, Yu (School of Mechanics Engineering, Harbin Institute of Technology, Harbin 150001, China); Zheng, Shutao; Han, Junwei Source: Nongye Jixie Xuebao/Transactions of the Chinese Society of Agricultural Machinery, v 41,

5、n 6, p 20-24, June 2010 Language: ChineseDatabase: Compendex Abstract  -  Detailed  -  Cited by in Scopus (1)3. A general dynamics and control model of a class of multi-DOF manipulators for active vibration controlYun, Yuan (Department of Electromechanica

6、l Engineering, Faculty of Science and Technology, University of Macau, Av. Padre Tomás Pereira, Taipa, Macao SAR, China); Li, Yangmin Source:Mechanism and Machine Theory, v 46, n 10, p 1549-1574, October 2011Database: Compendex Abstract  -  DetailedSelected Re

7、cords 阅读文摘：Record 1 from Compendex for: (Dynamics) WN KY) AND (Vibration) WN KY) AND (Control) WN KY), 2000-2012Uncertainty modeling of structural dynamics for robust vibration controlWang, Feng1; Li, Dao-Kui2; Lei, Yong-Jun2 Source: Zhendong yu Chongji/J

8、ournal of Vibration and Shock, v 28, n 10, p 126-131, October 2009; Language: Chinese; ISSN: 10003835;Publisher: Chinese Vibration Engineering SocietyAuthor affiliation:1.Computational Aerodynamics Institute, China Aerodynamics Research and Development Center, Mianyang 62100

9、0, China1College of Aerospace and Material Engineering, National University of Defense Technology, Changsha 410073, ChinaAbstract: A general synthesis frame for the design of robust controller used in structural vibration was developed. Robust control theory of unc

10、ertain linear systems was introduced firstly. Uncertainty modeling of structural dynamics was then analyzed. The uncertainties included unmodeled high order dynamics, modal parameter error and modeling error of actuators and sensors. And mathematical model of these uncertainties were

11、formulated properly. Finally, the vibration control problem was brought into the framework of robust control theory, and the stability and performance of a closed cycle system were insured as long as the model errors fell into the prescribed bounds. (12 refs.)Main Headi

12、ng: Control system stabilityControlled terms:  Linear systems  -  Mathematical models  -  Modal analysis  -  Robust control  -  Structural dynamics  -  System theory  -  Uncertainty analysis  -  Vibra

13、tion controlRecord 2 from Compendex for: (Dynamics) WN KY) AND (Vibration) WN KY) AND (Control) WN KY), 2000-2012Check record to add to Selected RecordsTitle:Stewart platform vibration control strategy based on dynamicsAuthors:Yang, Yu1 ; Zheng, Shutao1 ; Han, Junwei1Author affiliation:1School

14、of Mechanics Engineering, Harbin Institute of Technology, Harbin 150001, ChinaCorresponding author:Yang, Y. (dophy2180)Source title:Nongye Jixie Xuebao/Transactions of the Chinese Society of Agricultural MachineryAbbreviated source title:Nongye Jixie XuebaoVolume:41Issue:6Issue date:June 2010Publica

15、tion year:2010Pages:20-24Language:ChineseISSN:10001298CODEN:NUYCA3Document type:Journal article (JA)Publisher:Chinese Society of Agricultural Machinery, No. 1 Beishatan Deshengmen Wai, Beijing, 100083, ChinaAbstract:With heavy load and high center of gravity, the Stewart platform based on kinematics

16、 control strategy vibrated in one degree of freedom will cause the vibration in other degrees of freedom. To solve this problem, a vibration control strategy used in the position closed loop was presented based on the Stewart platform dynamics. According to this control strategy, the actuator force,

17、 calculated by the dynamics model, was used to control the platform vibration, and the control precision was improved. At last this vibration control strategy was validated with the Stewart platform in 15°pitch posture. Comparing the vibration response of the Stewart platform controlled by kine

18、matics and dynamics respectively, the results showed that the proposed control strategy could reduce the coupling vibration caused by the platform load effectively, and could achieve the precise vibration control in any platform pose.Number of references:12Main heading:SimulatorsControlled terms:Dyn

19、amics - Kinematics - Roads and streets - Vibration controlUncontrolled terms:Center of gravity - Closed loops - Control precision - Control strategies - Coupling vibration - Degree of freedom - Degrees of freedom - Dynamics models - Heavy loads - Kinematics and dynamics - Kinematics control - Multi-

20、body dynamic - ON dynamics - Shaking tables - Stewart platforms - Vibration - Vibration responseClassification code:931.1 Mechanics - 731.3 Specific Variables Control - 671 Naval Architecture - 662.1 Automobiles - 657.1 Solar Energy and Phenomena - 655.2 Satellites - 654.1 Rockets and Missiles - 621

21、 Nuclear Reactors - 406.2 Roads and StreetsDatabase:CompendexRecord 3 from Compendex for: (Dynamics) WN KY) AND (Vibration) WN KY) AND (Control) WN KY), 2000-2012Check record to add to Selected RecordsTitle:A general dynamics and control model of a class of multi-DOF manipulators for active vibratio

22、n controlAuthors:Yun, Yuan1 ; Li, Yangmin1Author affiliation:1Department of Electromechanical Engineering, Faculty of Science and Technology, University of Macau, Av. Padre Tomás Pereira, Taipa, Macao SAR, ChinaCorresponding author:Li, Y. (ymliumac.mo)Source title:Mechanism and Machine TheoryAb

23、breviated source title:Mech Mach TheoryVolume:46Issue:10Issue date:October 2011Publication year:2011Pages:1549-1574Language:EnglishISSN:0094114XCODEN:MHMTASDocument type:Journal article (JA)Publisher:Elsevier Ltd, Langford Lane, Kidlington, Oxford, OX5 1GB, United KingdomAbstract:A general dynamic m

24、odel of a class of parallel platforms for vibration control applications based on Kane's method is presented. A general parallel platform is composed of a moving platform, a base platform, and i limbs with identical kinematic structure. Each limb connects the mobile platform to the base platform

25、 by j + 1 hinges and j struts, where the prismatic actuator is fixed at one of the struts. The hinges can be replaced by any other kind of conventional hinges or flexure hinges. The control system architecture based on mixed H2/H synthesis method is introduced for a class of parallel platforms as a

26、multiple-input/multiple-output (MIMO) problem for the purpose of active vibration isolation. A case study is illustrated and the theoretical analysis is validated at last. © 2011 Elsevier Ltd. All rights reserved.Number of references:15Main heading:Fixed platformsControlled terms:Hinges - Mecha

27、nisms - Struts - Vibration controlUncontrolled terms:Active vibration controls - Active vibration isolation - Base platforms - Control system architecture - Flexure hinge - General dynamics - Kane's method - Kinematic structures - Mixed H - Mobile platform - Moving platform - Multi-DOF - Multipl

28、e input/multiple outputs - Parallel mechanism - Parallel platforms - Synthesis method - Vibration control applicationClassification code:408.2 Structural Members and Shapes - 511.2 Oil Field Equipment - 601.3 Mechanisms - 605 Small Tools and Hardware - 731.3 Specific Variables ControlDatabase:Compendex7、标示原文线索：用中文标示各检索结果的著录事项第一篇文献： 一、篇名：Uncertainty modeling of structural dynamics for robust vibration control二、第一责任者：Wang, F.三、作者简介：1Computational Aerodynamics Institute, China Aerodynamics Research and