期刊文献+

免疫反馈算法及其在航空发动机控制中的应用 被引量:2

Application of immune feedback mechanism on aeroengine control
下载PDF
导出
摘要 基于生物免疫系统的反馈机理,针对现有免疫反馈算法在系统超调后性能恶化的不足,提出了一种新型的免疫反馈算法。该算法考虑了系统超调后的免疫响应过程,补充给出了系统超调初期、中期及后期的免疫规则。仿真结果表明,基于新型免疫规则的PID控制器超调更小、响应更快,抗干扰能力强,十分适用于大惯性对象和超调量大的系统。 Based on immune feedback mechanism of biological immune system, a new immune feedback algorithm was carried out in order to overcome the disadvantages of present immune feedback algorithm in overshoot state. The response after overshoot was considered in the new algorithm, and the immune feedback rules of different period of response progress especially when overshoot was presented. Results show that the new immune PID controller has faster response, less overshoot and better ability of anti-amming, which is suitable for those system that has large inertia or overshoot.
出处 《推进技术》 EI CAS CSCD 北大核心 2008年第1期84-88,共5页 Journal of Propulsion Technology
关键词 航空发动机 免疫反馈 PID控制 SIMULINK Aircraft engine Immune feedback PID control Simulink
  • 相关文献

参考文献7

二级参考文献17

  • 1柳鲍穆得罗夫 陈琴 王金瑞译.相似理论在燃气涡轮发动机调节系统设计中的应用[M].北京:国防工业出版社,1975..
  • 2王琴芳.航空燃气涡轮发动机原理[M].南京:南京航空航天大学,1999..
  • 3范永胜,徐治皋,陈来九.基于动态特性机理分析的锅炉过热汽温自适应模糊控制系统研究[J].中国电机工程学报,1997,17(1):23-28. 被引量:205
  • 4Ying H,Automatica,1990年,26卷,3期,513页
  • 5Qi X M,Fuzzy Sets Systems,1997年,91卷,279页
  • 6Tang Z,Proc 27th Int Symp on Multiple- valued L ogic.Antigo-nish,1997年,233页
  • 7Choi K I,Kim S Y,Suo J S,et al. A Mathematical Model for the Estimation of Flue Temperature in a Coke Oven[A]. Ironmaking Conference Proceedings[C]. Chicago, 1997: 107-113.
  • 8Tarakanov A, Dasgupta D. A Formal Model of an Artificial Immune System[J]. Biosystems, 2000,55(3):15-18.
  • 9Sergei Gutnikov,Yuri Melnikov. A Simple Non-linear Model of Immune Response[J]. Chaos,Solitons and Fractals, 2003,16(1):125-132.
  • 10Qiao W Z, Mizumoto M. PID Type Fuzzy Controller and Parameters Adaptive Method[J]. Fuzzy Sets and Systems, 1996,78(1):23-35.

共引文献208

同被引文献16

引证文献2

二级引证文献4

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