Asteroid Rendezvous Mission Design Using Multiobjective Particle Swarm Optimization

<table class="table-group" width="800px"><tr class="fig-image" id="a"><td><img alt="823659.fig.008a" src="https://static.hindawi.com/articles/mpe/volume-2014/823659/figures/823659.fig.008a.jpg"/></td></tr><tr class="fig-caption"><td align="center"><table><tr><td><b>(a) </b>Asteroid 1, two-impulse</td></tr></table></td></tr><tr class="fig-image" id="b"><td><img alt="823659.fig.008b" src="https://static.hindawi.com/articles/mpe/volume-2014/823659/figures/823659.fig.008b.jpg"/></td></tr><tr class="fig-caption"><td align="center"><table><tr><td><b>(b) </b>Asteroid 2, two-impulse</td></tr></table></td></tr></table>

<table>Relations between total characteristic velocity, transfer time, and earth departure time.</table>

Mathematical Problems in Engineering

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Figure 8

Figure 8: Asteroid Rendezvous Mission Design Using Multiobjective Particle Swarm Optimization 