Optimal Lunar Landing Trajectory Design for Hybrid Engine

<table class="table-group" id="tab1"><tr><td><table class="table"><tr><td class="thead-hr" colspan="3"><hr/></td></tr><tr class="thead"><td align="left"> </td><td align="center">Final mass (kg)</td><td align="center">Total fuel consumption (kg)</td></tr><tr><td class="thead-hr" colspan="3"><hr/></td></tr><tr><td align="left">Previous optimal solution</td><td align="center">154.5413</td><td align="center">145.4587</td></tr><tr><td align="left">Proposed optimal solution</td><td align="center">160.6186</td><td align="center">139.3814</td></tr><tr class="table-tr"><td colspan="3"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

Mathematical Problems in Engineering

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Table 1

Table 1: Optimal Lunar Landing Trajectory Design for Hybrid Engine 