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基于粗集模型的歼击机损伤故障检测 被引量:3

Damage fault detection of fighter based on rough set model
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摘要 从粗集的观点出发,将歼击机的损伤故障信息表示为一种信息系统,进而表示为决策表的形式,然后利用粗集方法对决策表进行属性简化,提取决策规则,再利用规则完成歼击机的损伤故障检测.粗集方法可直接处理歼击机的可测输出信号,不需要对象的数学模型和相关先验知识.仿真结果表明了所提出方法的有效性和实用性. The information of aircraft's faults was denoted as a kind of information system based on rough set, and then as a decision table. Rough set based algorithms were applied to attributes reduction, rules extraction, fulfilling the detection of the damage faults. The proposed method dealt with measurable signal of the aircraft, mathematical model and no relevant transcendental knowledge was needed. The results of the simulation revealed the efficiency and practicality of this method.
出处 《控制理论与应用》 EI CAS CSCD 北大核心 2003年第6期943-946,共4页 Control Theory & Applications
基金 国家自然科学重点基金项目(60234010) 航空科学基金项目(02E52025).
关键词 歼击机 损伤故障 故障检测 粗集模型 信息表示 信息系统 决策规则 数学模型 rough set fault detection information system indiscernibility relation decision table
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参考文献4

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同被引文献14

  • 1刘守生,于盛林,丁勇.基于进化FCM算法的故障诊断方法[J].系统工程与电子技术,2004,26(9):1287-1290. 被引量:3
  • 2熊浩,张晓星,廖瑞金,常涛,孙才新.基于动态聚类的电力变压器故障诊断[J].仪器仪表学报,2007,28(3):456-459. 被引量:21
  • 3刘波,王凌,金以慧.差分进化算法研究进展[J].控制与决策,2007,22(7):721-729. 被引量:289
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  • 5YANG Wen-xian.Establishment of the mathematical model for diagnosing the engine valve faults by genetic programming[J].Journal of Sound and Vibration,2006,293(1-2):213-226.
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  • 7BREST J,ZUMER V,MAUCEC M S.Self-adaptive differential evolution algorithm in constrained real-parameter optimization[C]//Proc of IEEE Congress on Evolutionary Computation.Vancouver DC:IEEE Press,2006:215-221.
  • 8易德生,郭萍编著.灰色理论与方法[M]. 石油工业出版社, 1992
  • 9赵熙临,刘辉.粗糙集理论在故障诊断中的问题分析[J].计算机技术与发展,2008,18(1):132-135. 被引量:1
  • 10刘小雄,武燕,史静平,章卫国.一种故障诊断的贝叶斯优化算法研究[J].计算机应用研究,2009,26(1):129-131. 被引量:5

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