Optimization of Allocation and Launch Conditions of Multiple Missiles for Three-Dimensional Collaborative Interception of Ballistic Targets

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static.hindawi.com/articles/ijae/volume-2016/9582816/figures/9582816.fig.008a.svgz" name="9582816.fig.008a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Norm of the range-to-go estimation error versus time in terminal phase</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/ijae/volume-2016/9582816/figures/9582816.fig.008b.svgz" name="9582816.fig.008b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Norm of the line of sight estimation error versus time in terminal phase</td></tr><tr class="fig-image" id="c"><td><object data="https://static.hindawi.com/articles/ijae/volume-2016/9582816/figures/9582816.fig.008c.svgz" name="9582816.fig.008c" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(c) </b>Norm of the target acceleration estimation error versus time in terminal phase</td></tr></table>

<div>Filter performance versus time in terminal phase for intercepting high altitude-low velocity target.</div>

International Journal of Aerospace Engineering

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Figure 8

Figure 8: Optimization of Allocation and Launch Conditions of Multiple Missiles for Three-Dimensional Collaborative Interception of Ballistic Targets 

Figure 8 | Optimization of Allocation and Launch Conditions of Multiple Missiles for Three-Dimensional Collaborative Interception of Ballistic Targets 