Efficient Method of Firing Angle Calculation for Multiple Launch Rocket System Based on Polynomial Response Surface and Kriging Metamodels

<figure class="figure-group responsive"><div class="sub-figure" id="a"><object data="https://static-preview.hindawi.com/articles/mpe/volume-2019/7689860/figures/7689860.fig.007a.svgz" name="7689860.fig.007a" type="image/svg+xml"></object><div class="fig-label">(a) Overall distribution</div></div><div class="sub-figure" id="b"><object data="https://static-preview.hindawi.com/articles/mpe/volume-2019/7689860/figures/7689860.fig.007b.svgz" name="7689860.fig.007b" type="image/svg+xml"></object><div class="fig-label">(b) Partial amplification of P3 portion</div></div></figure>

<p>Distributions of the number of iterations merely considering the atmospheric pressure and virtual temperature.</p>

Mathematical Problems in Engineering

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Figure 7

Figure 7: Efficient Method of Firing Angle Calculation for Multiple Launch Rocket System Based on Polynomial Response Surface and Kriging Metamodels 