Vibration and Performance Analyses Using Individual Blade Pitch Controls for Lift-Offset Rotors

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static.hindawi.com/articles/ijae/volume-2019/9589415/figures/9589415.fig.001a.svgz" name="9589415.fig.001a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>XH-59A Technology Demonstrator [<a href="/journals/ijae/2019/9589415/#B2">2</a>]</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/ijae/volume-2019/9589415/figures/9589415.fig.001b.svgz" name="9589415.fig.001b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>X2 Technology Demonstrator [<a href="/journals/ijae/2019/9589415/#B2">2</a>]</td></tr><tr class="fig-image" id="c"><td><object data="https://static.hindawi.com/articles/ijae/volume-2019/9589415/figures/9589415.fig.001c.svgz" name="9589415.fig.001c" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(c) </b>S-97 Raider [<a href="/journals/ijae/2019/9589415/#B3">3</a>]</td></tr></table>

<div>Lift-offset helicopters using ABC™.</div>

International Journal of Aerospace Engineering

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Figure 1

Figure 1: Vibration and Performance Analyses Using Individual Blade Pitch Controls for Lift-Offset Rotors 