Generic Model of a Satellite Attitude Control System

<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">Description</td><td class="align_center">Value</td><td class="align_center">Unit</td></tr><tr><td class="thead-hr" colspan="3"><hr/></td></tr><tr><td class="align_left">Moment of inertia about spin axis</td><td class="align_center">51.16</td><td class="align_center">[kg·mm<sup>2</sup>]</td></tr><tr><td class="align_left">Armature current</td><td class="align_center">0.35</td><td class="align_center">[A]</td></tr><tr><td class="align_left">Viscous friction</td><td class="align_center">3.837</td><td class="align_center">[kg·mm<sup>2</sup>/s]</td></tr><tr><td class="align_left">Motor torque constant</td><td class="align_center">51.6393</td><td class="align_center">[°]</td></tr><tr class="table-tr"><td colspan="3"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

International Journal of Aerospace Engineering

tab3

Table 3

Table 3: Generic Model of a Satellite Attitude Control System 