Gust Load Alleviation including Geometric Nonlinearities Based on Dynamic Linearization of Structural ROM

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static.hindawi.com/articles/ijae/volume-2019/3207912/figures/3207912.fig.009a.svgz" name="3207912.fig.009a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Accelerometer and servo</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/ijae/volume-2019/3207912/figures/3207912.fig.009b.svgz" name="3207912.fig.009b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>MCU for servo</td></tr></table>

<div>Parts of hardware devices in a wind tunnel test [<a href="/journals/ijae/2019/3207912/#B32">32</a>].</div>

International Journal of Aerospace Engineering

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Figure 9

Figure 9: Gust Load Alleviation including Geometric Nonlinearities Based on Dynamic Linearization of Structural ROM 