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飞行器突发故障演化模型设计与仿真

韩治中 王仲生 姜洪开

计算机工程2012,Vol.38Issue(21):14-16,21,4.
计算机工程2012,Vol.38Issue(21):14-16,21,4.DOI:10.3969/j.issn.1000-3428.2012.21.004

飞行器突发故障演化模型设计与仿真

Design and Simulation of Sudden Failure Evolution Model on Aircraft

韩治中 1王仲生 1姜洪开1

作者信息

  • 1. 西北工业大学航空学院,西安710072
  • 折叠

摘要

Abstract

The aircraft sudden failure is a kind of random faults, which is a serious threat for the safe. To present the law of the aircraft sudden failure, this paper proposes to analyze and disclose the mechanism, the feature and procedure of the aircraft sudden failure evolution by dissipative structure theory. Based on that, it models the sudden failure evolution model on aircraft via time varying entropy and time varying frequency band energy distribution, and then it simulates the model by the surge of aero-engine. The results suggest that the entropy and the frequency band energy distribution of the dissipative structure are useful to present the procedure and the feature of the aircraft sudden failure evolution.

关键词

飞行器/突发故障/演化模型//耗散结构

Key words

aircraft/ sudden failure/ evolution model/ entropy/ dissipative structure

分类

信息技术与安全科学

引用本文复制引用

韩治中,王仲生,姜洪开..飞行器突发故障演化模型设计与仿真[J].计算机工程,2012,38(21):14-16,21,4.

基金项目

国家自然科学基金资助项目"飞行器突发故障演化规律及共防护方法研究"(51075330,50975231) (51075330,50975231)

计算机工程

OACSCDCSTPCD

1000-3428

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