A Convex Approach for Trajectory Optimization of Super-Synchronous-Transfer-Orbit Large Launch Systems with Time-Position Constraints

<table class="table-group" id="tab4"><tr><td><table class="table"><tr><td class="thead-hr" colspan="3"><hr/></td></tr><tr class="thead"><td class="align_left"></td><td class="align_center">Convex optimization</td><td class="align_center">NLP</td></tr><tr><td class="thead-hr" colspan="3"><hr/></td></tr><tr><td class="align_left">Flight time in LEO, s</td><td class="align_center">874.4</td><td class="align_center">874.2</td></tr><tr><td class="align_left">Flight time from LEO to SSTO, s</td><td class="align_center">355.6</td><td class="align_center">355.4</td></tr><tr><td class="align_left">CPU time, s</td><td class="align_center">2.48</td><td class="align_center">43.27</td></tr><tr class="table-tr"><td colspan="3"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>Comparison of simulation results.</div>

International Journal of Aerospace Engineering

tab4

Table 4

Table 4: A Convex Approach for Trajectory Optimization of Super-Synchronous-Transfer-Orbit Large Launch Systems with Time-Position Constraints 