Probabilistic Value-Centric Optimization Design for Fractionated Spacecrafts Based on Unscented Transformation

<table class="table-group" id="tab6"><tr><td><table class="table"><tr><td class="thead-hr" colspan="3"><hr/></td></tr><tr class="thead"><td align="left">Optimal conditions</td><td align="center">Lower bound</td><td align="center">Upper bound</td></tr><tr><td class="thead-hr" colspan="3"><hr/></td></tr><tr><td align="left">Orbit altitude (km)</td><td align="center">400</td><td align="center">700</td></tr><tr><td align="left">LTDN (hour)</td><td align="center">9</td><td align="center">13</td></tr><tr><td align="left">Number of modules (—)</td><td align="center">1</td><td align="center">6</td></tr><tr class="table-tr"><td colspan="3"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

Inequality constraints for the three variables.

Mathematical Problems in Engineering

tab6

Table 6

Table 6: Probabilistic Value-Centric Optimization Design for Fractionated Spacecrafts Based on Unscented Transformation 