Finite-Horizon Optimal Tracking Guidance for Aircraft Based on Approximate Dynamic Programming

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static.hindawi.com/articles/mpe/volume-2019/8649781/figures/8649781.fig.002a.svgz" name="8649781.fig.002a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Critic weight</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/mpe/volume-2019/8649781/figures/8649781.fig.002b.svgz" name="8649781.fig.002b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Actor weight</td></tr></table>

Mathematical Problems in Engineering

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Figure 2: Finite-Horizon Optimal Tracking Guidance for Aircraft Based on Approximate Dynamic Programming 