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

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static.hindawi.com/articles/sv/volume-2015/348971/figures/348971.fig.007a.svgz" name="348971.fig.007a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Response at the first 5 seconds</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/sv/volume-2015/348971/figures/348971.fig.007b.svgz" name="348971.fig.007b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Response at the last 5 seconds</td></tr></table>

<div>The comparison between the experimental response and the output of identified AR model.</div>

Shock and Vibration

fig7

Figure 7

Figure 7: GPC-Based Gust Response Alleviation for Aircraft Model Adapting to Various Flow Velocities in the Wind Tunnel 