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Operational Mode Identification Based on Sliding Time Window Method and Eigensystem Realization Algorithm

WANG Liang ZHANG Yan CAI Yipeng NANGONG Zijun

南京航空航天大学学报(英文版)2019,Vol.36Issue(5):838-844,7.
南京航空航天大学学报(英文版)2019,Vol.36Issue(5):838-844,7.

Operational Mode Identification Based on Sliding Time Window Method and Eigensystem Realization Algorithm

Operational Mode Identification Based on Sliding Time Window Method and Eigensystem Realization Algorithm

WANG Liang 1ZHANG Yan 1CAI Yipeng 1NANGONG Zijun1

作者信息

  • 1. China Academy of Launch Vehicle Technology,Beijing 100076,P. R. China
  • 折叠

摘要

关键词

mode identification/robust/eigensystem realization algorithm (ERA)/operational mode/damping ratio

Key words

mode identification/robust/eigensystem realization algorithm (ERA)/operational mode/damping ratio

分类

数理科学

引用本文复制引用

WANG Liang,ZHANG Yan,CAI Yipeng,NANGONG Zijun..Operational Mode Identification Based on Sliding Time Window Method and Eigensystem Realization Algorithm[J].南京航空航天大学学报(英文版),2019,36(5):838-844,7.

基金项目

This work was supported in part by the National Basic Research Program of China (No. JCKY2016203B032). (No. JCKY2016203B032)

南京航空航天大学学报(英文版)

OACSCDCSTPCD

1005-1120

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