Application of the Kalman Filter to Estimate the State of an Aerobraking Maneuver

<table class="table-group" id="tab3"><tr><td><table class="table"><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr class="thead"><td align="left">Description</td><td align="center">Value</td></tr><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr><td align="left">Apogee altitude (km)</td><td align="center">425,000</td></tr><tr><td align="left">Perigee altitude (km)</td><td align="center">125</td></tr><tr><td align="left">Mean anomaly (degrees)</td><td align="center">180</td></tr><tr class="table-tr"><td colspan="2"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

Mathematical Problems in Engineering

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Table 3

Table 3: Application of the Kalman Filter to Estimate the State of an Aerobraking Maneuver 