Approximate Solutions to Nonlinear Optimal Control Problems in Astrodynamics

<table class="table-group" id="tab2"><tr><td><table class="table"><tr><td class="thead-hr" colspan="4"><hr/></td></tr><tr class="thead"><td align="left">Problem</td><td align="center"><span style="width: 9.0124998px;"><svg height="14.7625" id="M170" style="vertical-align:-0.15048pt" version="1.1" viewbox="0 0 9.0124998 14.7625" width="9.0124998" xmlns="http://www.w3.org/2000/svg" xmlns:xlink="http://www.w3.org/1999/xlink">
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</svg></span></td><td align="center">Iter</td><td align="center">CPU time (s)</td></tr><tr><td class="thead-hr" colspan="4"><hr/></td></tr><tr><td align="left"><span style="width: 56.900002px;"><svg height="16.25" id="M171" style="vertical-align:-4.77652pt" version="1.1" viewbox="0 0 56.900002 16.25" width="56.900002" xmlns="http://www.w3.org/2000/svg" xmlns:xlink="http://www.w3.org/1999/xlink">
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q0 16 13.5 31.5t28.5 15.5q12 0 17 -11q5 -10 25 -10q22 0 57.5 36t89.5 111l-40 108q-22 58 -36 58q-21 0 -67 -57l-19 20q81 107 125 107q17 0 30 -22t39 -88l22 -55q68 92 108.5 128.5t74.5 36.5q20 0 32.5 -14t12.5 -30z" id="x1D465"></path></g>
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</svg></span></td><td align="center">0.5298</td><td align="center">22</td><td align="center">5.425</td></tr><tr><td align="left"><span style="width: 77.099998px;"><svg height="19.225" id="M172" style="vertical-align:-4.77652pt" version="1.1" viewbox="0 0 77.099998 19.225" width="77.099998" xmlns="http://www.w3.org/2000/svg" xmlns:xlink="http://www.w3.org/1999/xlink">
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</svg></span></td><td align="center">4.8665</td><td align="center">123</td><td align="center">41.831</td></tr><tr class="table-tr"><td colspan="4"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

International Scholarly Research Notices

tab2

Table 2

Table 2: Approximate Solutions to Nonlinear Optimal Control Problems in Astrodynamics 