Recursive subspace identification for in-flight modal analysis of airplanes

被引:0
|
作者
De Cock, Katrien [1 ]
Mercere, Guillaume [1 ]
De Moor, Bart [1 ]
机构
[1] Katholieke Univ Leuven, Dept Elect Engn ESAT SCD, B-3001 Louvain, Belgium
来源
Proceedings of ISMA2006: International Conference on Noise and Vibration Engineering, Vols 1-8 | 2006年
关键词
D O I
暂无
中图分类号
O42 [声学];
学科分类号
070206 ; 082403 ;
摘要
In this paper recursive subspace identification algorithms are applied to track the modal parameters of airplanes on-line during test flights. The ability to track changes in the damping ratios and the influence of the forgetting factor are studied through simulations.
引用
收藏
页码:1563 / 1577
页数:15
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