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

Table 6

Gust response alleviation result for varying frequencies and varying velocities.

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	0.03	0.01	0.01	0.02	0.05	0.09	0.14
1.5	0.02	0.01	0.01	0.02	0.03	0.06	0.09
2.0	0.03	0.02	0.02	0.03	0.05	0.09	0.14
2.5	0.02	0.01	0.01	0.02	0.03	0.06	0.09
3.0	0.04	0.03	0.03	0.03	0.05	0.09	0.15
3.5	0.03	0.02	0.02	0.02	0.03	0.07	0.12
4.0	0.05	0.04	0.04	0.03	0.05	0.12	0.23
4.5	0.04	0.03	0.03	0.02	0.04	0.10	0.20
5.0	0.07	0.05	0.06	0.03	0.07	0.20	0.39
5.5	0.05	0.04	0.05	0.02	0.05	0.16	0.31
6.0	0.07	0.06	0.08	0.03	0.08	0.27	0.52