Shock and Vibration / 2016 / Article / Tab 1

Research Article

Gust Load Alleviation with Robust Control for a Flexible Wing

Table 1

Flight conditions of LTI models.

MaDynamic pressure (kPa)

0.4102030405060
0.5102030405060
0.6102030405060
0.7102030405060

The italic numbers mean that these flight conditions are unstable.