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

Table 1

The open-loop wing tip acceleration data due to sinusoidal gust in the wind tunnel test.

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	0.10	0.11	0.12	0.17	0.17	0.18	0.18
1.5	0.21	0.35	0.29	0.28	0.29	0.40	0.42
2.0	0.70	0.69	0.79	0.70	0.79	0.83	0.86
2.5	0.55	0.47	0.80	1.09	0.89	1.30	0.91
3.0	0.42	0.61	0.85	1.28	1.34	1.56	1.82
3.5	0.35	0.37	0.54	1.26	1.24	1.28	1.69
4.0	0.39	0.46	0.73	1.23	1.40	1.80	2.16
4.5	0.32	0.44	0.61	1.06	0.91	1.28	1.82
5.0	0.34	0.42	0.70	0.86	1.32	1.52	1.93
5.5	0.27	0.34	0.49	1.36	0.99	1.49	2.16
6.0	0.33	0.41	0.53	1.41	1.23	1.97	2.48