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.0011a.svgz" name="3503870.fig.0011a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Aircraft speed and wheel speed</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/jece/volume-2017/3503870/figures/3503870.fig.0011b.svgz" name="3503870.fig.0011b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Running distance</td></tr><tr class="fig-image" id="c"><td><object data="https://static.hindawi.com/articles/jece/volume-2017/3503870/figures/3503870.fig.0011c.svgz" name="3503870.fig.0011c" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(c) </b>Brake pressure</td></tr></table>

<div>Simulation results when deceleration rate is 3.05.</div>

Journal of Electrical and Computer Engineering

fig11

Figure 11

Figure 11: Research on HILS Technology Applied on Aircraft Electric Braking System 