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浏览/检索结果: 共13条,第1-10条 帮助

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International Round-Robin Test of Critical Current of Superconducting Cable Sample 期刊论文  OAI收割
IEEE TRANSACTIONS ON APPLIED SUPERCONDUCTIVITY, 2024, 卷号: 34
作者:  
Matsushita, T.;  Kiuchi, M.;  Masuda, T.;  Mukoyama, S.;  Funaki, K.
  |  收藏  |  浏览/下载:10/0  |  提交时间:2024/11/20
Evaluation Method of Heavy-Ion-Induced Single-Event Upset in 3D-Stacked SRAMs 期刊论文  OAI收割
ELECTRONICS, 2020, 卷号: 9, 期号: 8, 页码: 14
作者:  
Zhao, Peixiong;  Liu, Tianqi;  Cai, Chang;  He, Ze;  Li, Dongqing
  |  收藏  |  浏览/下载:27/0  |  提交时间:2021/12/15
Laboratory investigation on strengthening behavior of frozen China standard sand 期刊论文  iSwitch采集
ACTA GEOTECHNICA, 2019, 卷号: 14, 期号: 1, 页码: 179-192
作者:  
Cai, Cong;  Ma, Wei;  Zhou, Zhiwei;  Mu, Yanhu;  Zhao, Shuping
收藏  |  浏览/下载:99/0  |  提交时间:2019/10/09
An appraisal method of dynamic interpolation error for high precision encoder (EI CONFERENCE) 会议论文  OAI收割
2011 International Conference on Electronics and Optoelectronics, ICEOE 2011, July 29, 2011 - July 31, 2011, Dalian, China
作者:  
Wan Q.-H.;  Liu C.-X.;  Liu C.-X.
收藏  |  浏览/下载:18/0  |  提交时间:2013/03/25
Modular aircraft simulation platform based on simulink (EI CONFERENCE) 会议论文  OAI收割
2010 IEEE International Conference on Mechatronics and Automation, ICMA 2010, August 4, 2010 - August 7, 2010, Xi'an, China
Chen C.-Q.; Ji Y.
收藏  |  浏览/下载:28/0  |  提交时间:2013/03/25
Aircraft simulation platform is the most important supporting technology in the aircraft development process. This simulation platform can be used for validating the design of subsystem and also it provides the necessary data for the Aircraft design. Wind has great impact on the flight parameter. In order to accurately simulate the wind model and calculate the flight parameters  a simulation modeling method for flight parameter simulation platform under wind field environment is established. Firstly  the various sub-systems which affecting flight parameters are analyzed  some mathematical models of the flight parameter simulation platform is established. Secondly  the atmospheric wind field is studied to analyze the impact on its trajectory. Then the model is built in the Simulink toolbox in the Matlab which is based on the principles of hierarchy and modularity  using C MEX S-function for the complex kinetic equations. Finally  when the models have been established  encapsulating models for several subsystem and assembling them for the Aircraft simulation platform based on the unified interface. The simulation tests (including the performance test of a certain gliding Aircraft  the wind influence test of a certain uncontrolled aircraft) prove the simulation capability of the platform  and its calculating step can reach 1 ms. Comparing simulation with field test data of a certain uncontrolled aircraft  it shows that the relative deviation of range is 0.47%  the relative deviation of maximal altitude is 2.1%. Taking relevant standards as a reference standard  it is demonstrated the platform is reliable  meets the engineering accuracy requirements. 2010 IEEE.  
Miniaturize photoelectric stable platform (EI CONFERENCE) 会议论文  OAI收割
2010 International Conference on Computer Application and System Modeling, ICCASM 2010, October 22, 2010 - October 24, 2010, Shanxi, Taiyuan, China
Xue W.-Q.; Wang Y.-Y.; Dai M.
收藏  |  浏览/下载:79/0  |  提交时间:2013/03/25
In order to reduce the size and weight of the gimbal in a traditional stable platform and correct the disadvantage in size of the payload  the paper first improves the gimbal which is an important component of a stable photoelectric platform  that also is an important factor in affecting the size and weight of a stability platform. In this paper  a closed-form solution of 3-DOF manipulator is designed according mechanical arm design principles. This manipulator is formed by a three joint axes whose extended line is intersected at one point. A standard orthogonal coordinate system is set up for each rod in the manipulator. And then  rotation transformation matrix expression is obtained. At last in this paper  the manipulator arm-shaped method for solving solutions is description  and also  each parameter of the gimbal is calculated when the photoelectric detection devices at bottom reach the expected position. Test results show that the photoelectric stability platform with gimbal we designed is smaller  lighter and simpler than that traditional. Also  the packaging and size of the photoelectric will not be affected with this open structure. 2010 IEEE.  
White-light spectral scanning interferometry for surface measurement system (EI CONFERENCE) 会议论文  OAI收割
6th International Symposium on Precision Engineering Measurements and Instrumentation, August 8, 2010 - August 11, 2010, Hangzhou, China
作者:  
Wang C.
收藏  |  浏览/下载:27/0  |  提交时间:2013/03/25
The paper introduces the white-light spectral scanning interferometry for surface measurement. This interferometry can be used to measure the roughness of both smooth surfaces and those with large step heights. This real-time surface measurement can be achieved using acousto-optic tuneable filtering (AOTF) technique without mechanical scanning. At first  the structure and principle of this interferometry is introduced. Then the algorithm of the surface roughness measurement is proposed. What's more  the experiment with standard test piece is conducted. Compared with the traditional laser-light interferometry  the data shows that the proposed method has a higher accuracy which is proved to be nano-scale. A conclusion is given at last in which the superiorities and the limitations of the proposed system were discussed. 2010 SPIE.  
Stein-type improved estimation of standard error under asymmetric LINEX loss function 期刊论文  OAI收割
STATISTICS, 2009, 卷号: 43, 期号: 2, 页码: 121-129
作者:  
Zou, Guohua;  Zeng, Jie;  Wan, Alan T. K.;  Guan, Zhong
  |  收藏  |  浏览/下载:22/0  |  提交时间:2018/07/30
藏文字库标准符合性自动检测方案设计与实现 期刊论文  OAI收割
中文信息学报, 2008, 卷号: 22, 期号: 3, 页码: 124-128
刘瀚猛; 芮建武; 白真龙; 吴健
  |  收藏  |  浏览/下载:29/0  |  提交时间:2010/08/24
湿H2S环境中金属材料腐蚀的研究 期刊论文  OAI收割
石油化工腐蚀与防护, 2007, 卷号: 24, 期号: 3, 页码: 22-25
作者:  
张万贞
  |  收藏  |  浏览/下载:5/0  |  提交时间:2024/01/08