GPC-Based Gust Response Alleviation for Aircraft Model Adapting to Various Flow Velocities in the Wind Tunnel

Table 4

Gust response alleviation result for varying frequencies and fixed velocity.

Frequency: Hz	Acceleration at 12 m/s : g	Acceleration at 14 m/s : g	Acceleration at 16 m/s : g	Acceleration at 18 m/s : g	Acceleration at 20 m/s : g	Acceleration at 22 m/s : g	Acceleration at 24 m/s : g
1.0	0.08		0.06			0.17	0.14
1.5	0.06	0.17	0.05	0.22	0.15	0.13	0.12
2.0	0.10	0.32	0.09	0.42	0.26	0.25	0.24
2.5	0.08	0.25	0.07	0.33	0.20	0.20	0.19
3.0	0.14	0.41	0.15	0.61	0.34	0.39	0.37
3.5	0.10	0.21	0.14	0.47	0.26	0.33	0.31
4.0	0.18	0.11	0.31	0.77	0.46	0.74	0.64
4.5	0.13	0.05	0.20	0.41	0.33	0.80	0.61
5.0	0.21	0.21	0.22	0.11	0.49		0.82
5.5	0.15	0.21	0.12	0.31	0.38	0.89	0.45
6.0	0.24	0.39	0.16	0.77	0.67	1.14	0.70