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The Design of Real-Time Communication System Based on RFM and MRG Real Time for EAST 期刊论文  OAI收割
IEEE TRANSACTIONS ON PLASMA SCIENCE, 2018, 卷号: 46, 期号: 6, 页码: 2267-2271
作者:  
Li, C. C.;  Ji, Z. S.;  Wang, F.;  Yuan, Q. P.;  Li, S.
  |  收藏  |  浏览/下载:22/0  |  提交时间:2019/11/12
Upgrade of EAST plasma control system for steady-state advanced operation 期刊论文  OAI收割
FUSION ENGINEERING AND DESIGN, 2018, 卷号: 129, 期号: 无, 页码: 109-114
作者:  
Yuan, Q. P.;  Tang, J. Y.;  Penaflor, B.;  Johnson, R.;  Wu, K.
  |  收藏  |  浏览/下载:81/0  |  提交时间:2019/08/26
Design and implementation of Electro-optical Countermeasure Hardware-in-the-loop simulation system based on HLA (EI CONFERENCE) 会议论文  OAI收割
2010 3rd International Conference on Advanced Computer Theory and Engineering, ICACTE 2010, August 20, 2010 - August 22, 2010, Chengdu, China
作者:  
Guo J.;  Cui S.;  Guo J.;  Li Y.;  Li Y.
收藏  |  浏览/下载:21/0  |  提交时间:2013/03/25
Focusing control system of photoelectric theodolite based on CAN bus (EI CONFERENCE) 会议论文  OAI收割
2010 2nd International Conference on Computer Engineering and Technology, ICCET 2010, April 16, 2010 - April 18, 2010, Chengdu, China
Mi Y.
收藏  |  浏览/下载:20/0  |  提交时间:2013/03/25
Design of CAN bus application layer protocol for aerocraft control system (EI CONFERENCE) 会议论文  OAI收割
2010 2nd International Conference on Industrial Mechatronics and Automation, ICIMA 2010, May 30, 2010 - May 31, 2010, Wuhan, China
作者:  
Zhang Y.;  Zhang H.;  Zhang H.;  Zhang W.;  Zhang W.
收藏  |  浏览/下载:34/0  |  提交时间:2013/03/25
A special Controller Area Network (CAN) bus application layer protocol is designed for the highly reliable communication of microcomputer-based systems in aerocraft control system by analyzing the practical time sequence of data transmission  data priority  data type and data function etc in this paper. Identifier distribution  data storage form  data type  data exchange method and fault handling mechanism of the application layer protocol are specified in detail in the background of a real aerocraft control system. At last a simulation platform based on CAN bus for aerocraft control system is built to validate the design. Experimental results show that this application layer protocol meets the requirements of data transmission reliability  real-time and high efficiency. The bus load rate is low and there is great room for expansion. 2010 IEEE.  
Design of CAN bus interface for photoelectric encoder in the spaceflight camera (EI CONFERENCE) 会议论文  OAI收割
4th International Symposium on Advanced Optical Manufacturing and Testing Technologies: Advanced Optical Manufacturing Technologies, November 19, 2008 - November 21, 2008, Chengdu, China
作者:  
Wan Q.-H.;  She R.-H.;  Sun Y.;  Sun Y.
收藏  |  浏览/下载:21/0  |  提交时间:2013/03/25
In order to make photoelectric encoder usable in a spaceflight camera which adopts CAN bus as the communication method  CAN bus interface of the photoelectric encoder is designed in this paper. CAN bus interface hardware circuit of photoelectric encoder consists of CAN bus controller SJA 1000  CAN bus transceiver TJA1050 and singlechip. CAN bus interface controlling software program is completed in C language. A ten-meter shield twisted pair line is used as the transmission medium in the spaceflight camera  and speed rate is 600kbps.The experiments show that: the photoelectric encoder with CAN bus interface which has the advantages of more reliability  real-time  transfer rate and transfer distance overcomes communication line's shortcomings of classical photoelectric encoder system. The system works well in automatic measuring and controlling system. 2009 SPIE.  
基于Web的远程实时监控系统 学位论文  OAI收割
工学硕士, 中国科学院自动化研究所: 中国科学院自动化研究所, 1999
郭方路
收藏  |  浏览/下载:60/0  |  提交时间:2015/09/02