A Time-Domain Active Vibration Control Algorithm for Helicopter Based on a Prior Error Channel Identification Strategy

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static.hindawi.com/articles/sv/volume-2018/2870896/figures/2870896.fig.0012a.svgz" name="2870896.fig.0012a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Yang’s method</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/sv/volume-2018/2870896/figures/2870896.fig.0012b.svgz" name="2870896.fig.0012b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Proposed method</td></tr></table>

<div>Performance comparison between Yang’s method and the proposed method with error channel variation.</div>

Shock and Vibration

fig12

Figure 12

Figure 12: A Time-Domain Active Vibration Control Algorithm for Helicopter Based on a Prior Error Channel Identification Strategy 