Journals
Publish with us
Publishing partnerships
About us
Blog
Shock and Vibration
Journal overview
For authors
For reviewers
For editors
Table of Contents
Special Issues
Shock and Vibration
/
2016
/
Article
/
Tab 2
/
Research Article
Gust Load Alleviation with Robust Control for a Flexible Wing
Table 2
Open-loop flutter parameters.
Ma
-method
LTI model
LPV model
NPV model
, m/s
, Hz
, m/s
, Hz
, m/s
, Hz
, m/s
, Hz
0.4
154.3
30.22
154.8
31.69
121.7
100.67
152.3
31.52
0.5
183.3
28.52
185.6
28.82
152.1
100.51
185.5
28.85
0.6
211.0
26.39
214.5
26.12
214.7
26.49
214.5
26.13
0.7
238.1
23.93
242.4
23.97
247.9
24.51
241.8
23.15
The italic numbers mean that these results are unacceptable.