Modified Chebyshev-Picard Iteration Methods for Station-Keeping of Translunar Halo Orbits

<table class="table-group" width="800px"><tr class="fig-image" id="a"><td><img alt="926158.fig.007a" src="https://static.hindawi.com/articles/mpe/volume-2012/926158/figures/926158.fig.007a.jpg"/></td></tr><tr class="fig-caption"><td align="center"><table><tr><td><b>(a) </b>Averaged total impulses</td></tr></table></td></tr><tr class="fig-image" id="b"><td><img alt="926158.fig.007b" src="https://static.hindawi.com/articles/mpe/volume-2012/926158/figures/926158.fig.007b.jpg"/></td></tr><tr class="fig-caption"><td align="center"><table><tr><td><b>(b) </b>Averaged maximum deviation</td></tr></table></td></tr><tr class="fig-image" id="c"><td><img alt="926158.fig.007c" src="https://static.hindawi.com/articles/mpe/volume-2012/926158/figures/926158.fig.007c.jpg"/></td></tr><tr class="fig-caption"><td align="center"><table><tr><td><b>(c) </b>Averaged mean deviation</td></tr></table></td></tr></table>

<table>Performance versus coefficient of control.</table>

Mathematical Problems in Engineering

fig7

Figure 7

Figure 7: Modified Chebyshev-Picard Iteration Methods for Station-Keeping of Translunar Halo Orbits 