Cooperative Guidance of Seeker-Less Missiles for Precise Hit

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static.hindawi.com/articles/ijae/volume-2019/8939213/figures/8939213.fig.005a.svgz" name="8939213.fig.005a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>1st modified two-stage guidance law</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/ijae/volume-2019/8939213/figures/8939213.fig.005b.svgz" name="8939213.fig.005b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>2nd modified two-stage guidance law</td></tr></table>

<div>Normal acceleration command for modified guidance laws.</div>

International Journal of Aerospace Engineering

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Figure 5

Figure 5: Cooperative Guidance of Seeker-Less Missiles for Precise Hit 