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

<table class="table-group" id="tab3"><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">942.2</td><td class="align_center">942.3</td></tr><tr><td class="align_left">Flight time from LEO to SSTO, s</td><td class="align_center">527.8</td><td class="align_center">527.6</td></tr><tr><td class="align_left">CPU time, s</td><td class="align_center">2.23</td><td class="align_center">38.34</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

tab3

Table 3

Table 3: A Convex Approach for Trajectory Optimization of Super-Synchronous-Transfer-Orbit Large Launch Systems with Time-Position Constraints 