Research Article

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

Table 2

Alleviation result for different length of prediction steps.

Case numberLength of prediction and control stepsOpen-loop acceleration: gClosed-loop acceleration: gAlleviation factor

Case  1, 0.8580.8234.1%
Case  2, 0.8580.37156.8%
Case  3, 0.8580.1187.2%