期刊文献+

非相似余度作动系统建模研究 被引量:6

Modeling and Analysis of the Dissimilar Redundant Actuator System
下载PDF
导出
摘要 为了提高伺服作动系统的可靠性,设计了一种非相似余度作动系统,建立了非相似余度作动系统的数学模型,并分析了系统的性能。结果表明,非相似余度作动系统的动态性能比单通道工作时有所提高,在一个通道发生故障时,仍然能够正常工作。 In order to improve the reliability of servo systems, a dissimilar redundant servo actuator system was designed. The mathematical model of the system was estabhshed. The performances of the system was analyzed. The results prove that the dynamic performance of the dissimilar redundant actuator system is improved compared with the single channel system, and when one channel failed, the system could still work properly.
出处 《机床与液压》 北大核心 2008年第6期79-81,共3页 Machine Tool & Hydraulics
关键词 作动系统 非相似余度 数学模型 动态性能 Actuator system Dissimilar redundancy Mathematical model Dynamic performance
  • 相关文献

参考文献2

二级参考文献4

  • 1Huszerl G, Majzik I. Modeling and Analysis of Redundancy Management in Distributed Object-oriented Systems by Using UML Statecharts [A]. Euromicro Conf Proc 27th[C]. Budapest, 2001 : 200-207.
  • 2Yao Y P, Cheng M H. The Application on Dynamic Fault tree Analysis for Dissimilar Fault-tolerant Flight Control System [A]. AIAA/IEEE Digital Avionics Systems Conf Proc[C]. St Louis, MO, 1999,1 : 3. B. 1-1-3. B. 1-6.
  • 3Ereau J F. Petri Nets for the Evaluation of Redundant Systems[J]. Reliability Engineering & System Safety,1997,55 (2) : 95-104.
  • 4Yeh Y C. Triple - Triple Redundant 777 Primary Flight Computer[A]. Aerospace Applications Conf[C].Aspen, Co, 1996, (1) :293-307.

共引文献33

同被引文献29

  • 1范同春,王继林,王兰普.液压油污染对波音777飞机扰流板PCU励磁电路的影响[J].航空维修与工程,2004(6):49-50. 被引量:1
  • 2陈宗基,秦旭东,高金源.非相似余度飞控计算机[J].航空学报,2005,26(3):320-327. 被引量:41
  • 3王非.飞控计算机余度结构与设计策略研究[J].航空计算技术,1996,26(1):1-4. 被引量:7
  • 4程涛,王占林.灵巧式舵机并行驱动的研究[J].北京航空航天大学学报,1996,22(2):167-170. 被引量:8
  • 5Bennett J W, Mecrow B C, Jack A G,et al. A prototype electrical actuator for aircraft flaps[ J]. IEEE Transactions on Industry Ap- plications, 2010,46 ( 3 ) :915 - 921.
  • 6Garcia A, Cusido J, Rosero J A, et al. Reliable electro-mechanical actuators in aircraft[J]. IEEE Aerospace and Electronic Systems Magazine ,2008,23 ( 8 ) : 19 - 25.
  • 7Bennett J W, Mecrow B C,Atkinson D J. Safety-critical design of electromechanical actuation systems in commercial aircraft [ J ]. lET Electric Power Applications,2011,5 ( 1 ) :37 - 47.
  • 8Qi Haitao, Mare J C, Fu Yongling. Force equalization in hybrid actuation systems[ C ]//Proceedings of the Seventh International Conference on Fluid Power Transmission and Control. Hangzhou : World Publishing Corporation,2009:342 - 348.
  • 9Mare J C ,Moulaire P. The decoupling of position controlled electrohydraulic actuators mounted in tandem or in series[ C ]//Proceedings of the Seventh Scandinavian International Conference on Fluid Power. Linkoping: Linkoping Universitet Institute of Technology ,2001:93 - 99.
  • 10Jacazio G, Gastaldi L. Equalization techniques for dual redundant electro hydraulic servo actuators for flight control systems [ C ]// ASME Symposium on Fluid Power and Motion Control. Bath:American Society of Mechanical Engineers,2008:543 -549.

引证文献6

二级引证文献43

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