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-methodLTI modelLPV modelNPV model
, m/s, Hz, m/s, Hz, m/s, Hz, m/s, Hz

0.4154.330.22154.831.69121.7100.67152.331.52
0.5183.328.52185.628.82152.1100.51185.528.85
0.6211.026.39214.526.12214.726.49214.526.13
0.7238.123.93242.423.97247.924.51 241.823.15

The italic numbers mean that these results are unacceptable.