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Shock and Vibration
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Shock and Vibration
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2016
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Article
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Tab 1
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Research Article
Gust Load Alleviation with Robust Control for a Flexible Wing
Table 1
Flight conditions of LTI models.
Ma
Dynamic pressure
(kPa)
0.4
10
20
30
40
50
60
0.5
10
20
30
40
50
60
0.6
10
20
30
40
50
60
0.7
10
20
30
40
50
60
The italic numbers mean that these flight conditions are unstable.