期刊文献+

基于CAN总线的开放式网络数控系统研究 被引量:7

A CAN - Based Open - Architecturd CNC System
下载PDF
导出
摘要 在比较国内不同数控系统联网能力的基础上,对基于CAN总线局域网的新型开放式数控系统进行了研究,为进一步开发FMS和CIMS产品奠定了一定的技术基础。 On copmaring the abilities of being linked to the network of domsetic various CNC systems, in this paper, a new CAN based open - architectured CNC system is Researched. It is a certain technical base of developing FMS and CIMS products.
出处 《机电工程》 CAS 2000年第3期46-48,共3页 Journal of Mechanical & Electrical Engineering
基金 国家863计划CIMS领域资助项目!(863-511-943-002) 国家自然科学基金重点资助项目!(59635170)
关键词 CAN总线 开放式数控系统 局域网 FMS CIMS CAN - bus network open - architectured CNC DSP
  • 相关文献

参考文献4

二级参考文献4

共引文献34

同被引文献42

  • 1Sisson,Patterson B Faymon, David K. Digital Control Brings Large Turbofan Benefits to the Regional Jetliner Turbofan Market [J]. American Society of Mechanical Engineers(Paper), 1994,6 : 13- 16. 被引量:1
  • 2Carlson R J, West P M. Azouz D E. Digital Control System Development for an Intercooled Recuperated Gas Turbine[J].American Society of Mechanical Engineers (Paper), 1993,5 :24-27. 被引量:1
  • 3Gridley, Marvin C. Walker, Steven H. Inlet and Nozzle Technology for 21st Century Fighter Aircraf [J]. American Society of Mechanical Engineers (Paper), 1996,6 : 10- 13. 被引量:1
  • 4Egorov I N, Kreitinin G V. Optimum Control of Variable Components in Aircraft Gas Turbine Engines under Non Stationary Flow Disturbances at the Inlet[J]. American Society of Mechanical Engineers (Paper), 19 9 4,6 : 13 - 16. 被引量:1
  • 5Balakrishnan S R. Evolution of Control Systems for Aircraft Gas Turbine Engines under Development[J]. Journal of the Aeronautical Society of India, 1996,48 ( 1 ) : 96. 被引量:1
  • 6Schley W R. Distributed Flight Control and Propulsion Control Implementation Issues and Lessons Learned [J]. Journalof Engineering for Gas Turbines and Power, January, 1999,121:96-101. 被引量:1
  • 7Shaffer P L. Distributed Control Systems for Turbine Engines[J]. Journal of Engineering for Gas Turbines and Power,January, 1999,121 : 102- 107. 被引量:1
  • 8Fletcher T R. Convenient Airborne MIL-STD 1553 multiplex Data Bus Data Acquisition System[J]. Canadian Aeronautics and Space Journal, Dec, 1993,39 (4) : 185 - 190. 被引量:1
  • 9Thompson H A,et al. A CANbus-Based Safety-Critical Distributed Aeroengine Control Systems Architecture Demonstrator [J]. Microprocessors and Microsystems, 1999, 23.-345-355. 被引量:1
  • 10Kurt Sobanski,et al. Gas Turbine Distributed Control Systems: Power Supply and Communication Data Bus Design Considerations[R]. ASME 98-GT-414, The InternationalGas Turbine & Aeroengine Congress &Exhibition Stockholm, Sweden, June, 1998. 被引量:1

引证文献7

二级引证文献65

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部