期刊文献+

飞行器助推段振动环境分析 被引量:3

Analysis of nonstationary random vibration data during lift-off
下载PDF
导出
摘要 对飞行器助推段非平稳随机振动信号采用局部平稳模型进行分析,把此段非平稳随机信号的时变谱分解成2个独立的过程:决定时变均方值的确定性过程和决定频率特性的平稳随机过程.利用小波分析对确定性信号和随机信号进行分离,用信号的全部带宽计算非平稳信号的时变均方值,缩短了平均时间,减少了偏置误差;用信号的整个持续时间确定非平稳信号的谱特性,提高了频率分辨率,减少了随机误差.对分离出的平稳随机振动自功率谱密度进行了归纳,得到了飞行器助推段的振动环境. The locally stationary bration environment of aircraft during parametric model was established to analyze the nonstationary random vilift-off. The computation of a time-varying spectrum was decomposed into two separate operations, one to define the time-varying mean square value of the signal, and the other to define the spectral properties of the signal. The wavelet transforms were used to separate the nonstationary vibration signal into the deterministic signal and random signal. Specifically, the time-varying mean square value of the signal was computed using the entire signal bandwidth, and the averaging time could be made short without causing a large bias error. Conversely, the basic spectra character of the signal was computed using the entire signal duration, and the frequency resolution bandwidth could be made small without causing a large random error. The vibration environment of aircraft during lift-off was obtained by concluding the auto-spectra of stationary random vibration.
出处 《北京航空航天大学学报》 EI CAS CSCD 北大核心 2006年第7期760-763,共4页 Journal of Beijing University of Aeronautics and Astronautics
关键词 随机振动 小波变换 非平稳 random vibration wavelet transforms nonstationary
  • 相关文献

参考文献6

  • 1Piersol A G.Optimum data analysis procedures for TITAN IV and space shuttle payload acoustic measurements during lift-off[R].NASA-CR-190479,1991
  • 2黄怀德.振动工程[M].北京:宇航出版社,1993.10-39.
  • 3Himelblau H,Piersol A G.Handbook for dynamic data acquisition and analysis[M].Oxford:Institute of Environmental Sciences,1993:291
  • 4贝达特JS 皮尔索AG 凌福根 译.随机数据分析方法[M].北京:国防工业出版社,1976.86-182.
  • 5HB/Z87-84.飞机飞行振动环境测量数据的归纳方法[S].[S].,1985..
  • 6GJB/Z126-99,振动冲击、环境测量数据归纳方法[S]

共引文献17

同被引文献28

  • 1黄永安,邓子辰.Decentralized Sliding Mode Control for a Spacecraft Flexible Appendage Based on Finite Element Method[J].Chinese Journal of Aeronautics,2005,18(3):230-236. 被引量:2
  • 2张龙,熊国良,柳和生,邹慧君,陈慧.时变参数模型及其在非平稳振动分析中的应用[J].振动与冲击,2006,25(6):49-53. 被引量:9
  • 3Grenier Y. Time-Dependent ARMA Modeling of Non-Stationary Signals [J]. IEEE Trans. ASS-P, 1983,31:899-911.
  • 4Rao T S. The Fitting of Non-Stationary TimeSeries Models with Time Dependent Parame-ters [J]. J Royal Statist. Soc. Series B, 1970,32 (2).
  • 5Slepian D. Prolate Spheroidal Wave Function Fourier Analysis and Uncertainty[J]. Part Ⅴ:The Discrete Case. Bell System Tech. J. , 1978,57 ( 5 ) : 1371-1430.
  • 6Grenier Y. Time-Dependent ARMA Modeling of Non-Stationary Signals [J]. IEEE Trans. AS-SP, 1983,31:899-911.
  • 7Rao T S. The Fitting of Non-Stationary Time-Series Models with Time Dependent Parame-ters [ J ]. J Royal Statist. Soc. Series B,1970,32(2).
  • 8He Xingui, Liang Jiuzher. Process Neural Network. World Computer congress 2000, Proceedings of Conference on Intelligent In-formation Processing. August 2000. 143 146.
  • 9Kayhan A S, EI-Jaroudi A, Chaparro L F. Da-taAdaptive Evolutlonary Spectral Estimation[ J]. IEEE Trans. on Signal Processing, 1995,43 ( 1 ) :204-213.
  • 10Konzin F, Nakajima F. The Order Determination Problem for Linear Time-Varying AR Models [ J ]. IEEE Trans. on Automatic Contral, 1980,25 (2) :250-257.

引证文献3

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