Research Article
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 |
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