Nonsingular Continuous Finite-Time Convergent Guidance Law with Impact Angle Constraints

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2019/6024240/figures/6024240.fig.006a.svgz" name="6024240.fig.006a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Trajectories</td></tr><tr class="fig-image" id="b"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2019/6024240/figures/6024240.fig.006b.svgz" name="6024240.fig.006b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Missile accelerations</td></tr><tr class="fig-image" id="c"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2019/6024240/figures/6024240.fig.006c.svgz" name="6024240.fig.006c" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(c) </b>LOS angles</td></tr><tr class="fig-image" id="d"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2019/6024240/figures/6024240.fig.006d.svgz" name="6024240.fig.006d" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(d) </b>LOS angular rates</td></tr></table>

<div>Simulation results of comparison.</div>

International Journal of Aerospace Engineering

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Figure 6

Figure 6: Nonsingular Continuous Finite-Time Convergent Guidance Law with Impact Angle Constraints 