Attitude Active Disturbance Rejection Control of the Quadrotor and Its Parameter Tuning

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static.hindawi.com/articles/ijae/volume-2020/8876177/figures/8876177.fig.004a.svgz" name="8876177.fig.004a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Classical differentiator output tracking signal and differential signal</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/ijae/volume-2020/8876177/figures/8876177.fig.004b.svgz" name="8876177.fig.004b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Output tracking signal and differential signal of TD</td></tr></table>

International Journal of Aerospace Engineering

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Figure 4

Figure 4: Attitude Active Disturbance Rejection Control of the Quadrotor and Its Parameter Tuning 