Firing Control Optimization of Impulse Thrusters for Trajectory Correction Projectiles

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static.hindawi.com/articles/ijae/volume-2015/781472/figures/781472.fig.0010a.svgz" name="781472.fig.0010a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>CEP versus number of thrusters and individual thruster impulse</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/ijae/volume-2015/781472/figures/781472.fig.0010b.svgz" name="781472.fig.0010b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>CEP versus total impulse of thrusters and individual thruster impulse</td></tr><tr class="fig-image" id="c"><td><object data="https://static.hindawi.com/articles/ijae/volume-2015/781472/figures/781472.fig.0010c.svgz" name="781472.fig.0010c" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(c) </b>Maximal total attack angle versus individual thruster impulse and minimum firing interval</td></tr></table>

<div>The impact of parameters of thrusters on CEP and flight stability of rockets.</div>

International Journal of Aerospace Engineering

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Figure 10

Figure 10: Firing Control Optimization of Impulse Thrusters for Trajectory Correction Projectiles 