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基于Measurement Studio的民机颤振试飞数据实时监控分析系统设计与研究
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  • 英文篇名:Design and Research of Real-time Monitoring and Analysis System for Civil Aircraft Flutter Data Based on Measurement Studio
  • 作者:毛为 ; 刘涛 ; 陈家益 ; 高祥 ; 梁嘉弈
  • 英文作者:MAO Wei;LIU Tao;CHEN Jiayi;GAO Xiang;LIANG Jiayi;COMAC Flight Test Center;
  • 关键词:颤振 ; Measurement ; Studio ; 实时分析 ; DataBinding
  • 英文关键词:flutter;;Measurement Studio;;real-time analysis;;DataBinding
  • 中文刊名:MYFJ
  • 英文刊名:Civil Aircraft Design & Research
  • 机构:中国商飞民用飞机试飞中心;
  • 出版日期:2019-06-30
  • 出版单位:民用飞机设计与研究
  • 年:2019
  • 期:No.133
  • 基金:大型民机试飞数据高速实时处理及异常状态检测分析平台(17511105000)
  • 语种:中文;
  • 页:MYFJ201902008
  • 页数:5
  • CN:02
  • ISSN:31-1614/V
  • 分类号:17-21
摘要
颤振试飞是风险极高、多学科交叉的复杂试飞科目,其实时监控及分析显得极为重要。以某型国产民机颤振试飞为背景,基于Measurement Studio平台,设计开发了颤振试飞数据实时监控分析系统。系统集成了半带宽法、快速傅里叶变换、小波转换等算法,实现了颤振数据的时频域分析、阻尼计算,并以文本格式在实时状态下记录了颤振数据,同时以多线程和DataBinding模型完成了分析结果的实时显示,为国产民机的安全试飞提供了技术保障。
        Flutter flight test is highly risky,and it is a complex experiment with multidisciplinary crossover. Its real-time monitoring and analysis is extremely important. Based on the domestic civil aircraft flutter test,this paper designs and develops a real-time monitoring and analysis system using the Measurement Studio platform. The system integrates algorithms such as half-bandwidth method,fast Fourier transform and wavelet transform to realize timefrequency domain analysis and damping calculation of flutter data. In addition,the system records flutter data in real-time with text format. At the same time,the system completes the real-time display of the analysis results with multithreading and Data Binding model,which can provide technical support for the safe flight test of domestic civil aircraft.
引文
[1]陈奎孚,焦群英.某型飞机颤振试飞数据的模态参数识别[J].航空学报,2003,24(6):526-530.
    [2]卢晓东,霍幸莉,梁海州.民用飞机颤振试飞技术研究[J].航空工程进展,2014,5(1):80-84.
    [3]刘铁猛.深入浅出WPF[M].北京:中国水利水电出版社,2010:35-50.
    [4]Matthew MacDonald. WPF编程宝典[M].王德才,译.北京,清华大学出版社,2013:17-25.

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