Second-Order Sliding Mode Guidance Law considering Second-Order Dynamics of Autopilot

<figure class="figure-group responsive"><div class="sub-figure" id="a"><object data="https://static.hindawi.com/articles/jcse/volume-2019/8573140/figures/8573140.fig.002a.svgz" name="8573140.fig.002a" type="image/svg+xml"></object><div class="fig-label">(a) Target uniform motion</div></div><div class="sub-figure" id="b"><object data="https://static.hindawi.com/articles/jcse/volume-2019/8573140/figures/8573140.fig.002b.svgz" name="8573140.fig.002b" type="image/svg+xml"></object><div class="fig-label">(b) Target circular maneuver</div></div><div class="sub-figure" id="c"><object data="https://static.hindawi.com/articles/jcse/volume-2019/8573140/figures/8573140.fig.002c.svgz" name="8573140.fig.002c" type="image/svg+xml"></object><div class="fig-label">(c) Target sinusoidal maneuver</div></div></figure>

<p>The trajectories of missile and target.</p>

Journal of Control Science and Engineering

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Figure 2

Figure 2: Second-Order Sliding Mode Guidance Law considering Second-Order Dynamics of Autopilot 