A New Method for Initial Parameters Optimization of Guided Projectiles

<table class="table-group" width="800px"><tr class="fig-image" id="a"><td><img alt="486020.fig.003a" src="https://static.hindawi.com/articles/ijae/volume-2013/486020/figures/486020.fig.003a.jpg"/></td></tr><tr class="fig-caption"><td align="center"><table><tr><td><b>(a) </b>Comparison of height and range to target</td></tr></table></td></tr><tr class="fig-image" id="b"><td><img alt="486020.fig.003b" src="https://static.hindawi.com/articles/ijae/volume-2013/486020/figures/486020.fig.003b.jpg"/></td></tr><tr class="fig-caption"><td align="center"><table><tr><td><b>(b) </b>Comparison of velocity and path angle</td></tr></table></td></tr><tr class="fig-image" id="c"><td><img alt="486020.fig.003c" src="https://static.hindawi.com/articles/ijae/volume-2013/486020/figures/486020.fig.003c.jpg"/></td></tr><tr class="fig-caption"><td align="center"><table><tr><td><b>(c) </b>Comparison of AOA</td></tr></table></td></tr><tr class="fig-image" id="d"><td><img alt="486020.fig.003d" src="https://static.hindawi.com/articles/ijae/volume-2013/486020/figures/486020.fig.003d.jpg"/></td></tr><tr class="fig-caption"><td align="center"><table><tr><td><b>(d) </b>Comparison of overloading</td></tr></table></td></tr></table>

<table>Comparison of flight characteristics of projectile in different initial condition.</table>

International Journal of Aerospace Engineering

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Figure 3

Figure 3: A New Method for Initial Parameters Optimization of Guided Projectiles 