Low-Thrust Out-of-Plane Orbital Station-Keeping Maneuvers for Satellites

<table class="table-group" id="tab8"><tr><td><table class="table"><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr><td align="left">Semimajor axis</td><td align="center">0.50 Km</td></tr><tr><td align="left">Eccentricity</td><td align="center">0.005</td></tr><tr><td align="left">Inclination</td><td align="center">0.001 deg</td></tr><tr class="table-tr"><td colspan="2"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

Errors allowed for final keplerian elements for Maneuver 3.

Mathematical Problems in Engineering

tab8

Table 8

Table 8: Low-Thrust Out-of-Plane Orbital Station-Keeping Maneuvers for Satellites 