Multiple Gravity Assist Spacecraft Trajectories Design Based on BFS and EP_DE Algorithm

<table class="table-group" id="tab14"><tr><td><table class="table"><tr><td class="thead-hr" colspan="6"><hr/></td></tr><tr class="thead"><td class="align_left">Population</td><td class="align_center">Generation</td><td class="align_center">Optimal value (change in semimajor axis)</td><td class="align_center">Worst value</td><td class="align_center">Standard deviation</td><td class="align_center">Independent runs</td></tr><tr><td class="thead-hr" colspan="6"><hr/></td></tr><tr><td class="align_left">2000</td><td class="align_center">2000</td><td class="align_center"><span style="width: 92.1585ptpx;"><svg height="8.69875pt" id="M167" style="vertical-align:-0.3499298pt" version="1.1" viewbox="-0.0498162 -8.34882 92.1585 8.69875" width="92.1585pt" xmlns="http://www.w3.org/2000/svg" xmlns:xlink="http://www.w3.org/1999/xlink"><g transform="matrix(.013,0,0,-0.013,0,0)"><path d="M535 230V280H52V230H535Z" id="g117-33"></path><glyph.data ascent="3473" descent="-2876" horiz-adv-x="587" 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International Journal of Aerospace Engineering

tab14

Table 14

Table 14: Multiple Gravity Assist Spacecraft Trajectories Design Based on BFS and EP_DE Algorithm 