Research on HILS Technology Applied on Aircraft Electric Braking System

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static.hindawi.com/articles/jece/volume-2017/3503870/figures/3503870.fig.0015a.svgz" name="3503870.fig.0015a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Running distance</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/jece/volume-2017/3503870/figures/3503870.fig.0015b.svgz" name="3503870.fig.0015b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Aircraft speed</td></tr><tr class="fig-image" id="c"><td><object data="https://static.hindawi.com/articles/jece/volume-2017/3503870/figures/3503870.fig.0015c.svgz" name="3503870.fig.0015c" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(c) </b>Wheel speed</td></tr><tr class="fig-image" id="d"><td><object data="https://static.hindawi.com/articles/jece/volume-2017/3503870/figures/3503870.fig.0015d.svgz" name="3503870.fig.0015d" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(d) </b>Actual brake pressure</td></tr><tr class="fig-image" id="e"><td><object data="https://static.hindawi.com/articles/jece/volume-2017/3503870/figures/3503870.fig.0015e.svgz" name="3503870.fig.0015e" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(e) </b>Given brake pressure</td></tr></table>

<div>HILS results when deceleration rate is 2.1.</div>

Journal of Electrical and Computer Engineering

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Figure 15

Figure 15: Research on HILS Technology Applied on Aircraft Electric Braking System 