Attitude Maneuvering and Vibration Reducing Control of Flexible Spacecraft Subject to Actuator Saturation and Misalignment

<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 class="align_left"> </td><td class="align_center">Natural frequency (rad/s)</td><td class="align_center">Damping</td></tr><tr><td class="thead-hr" colspan="3"><hr/></td></tr><tr><td class="align_left">Mode 1</td><td class="align_center">1.0973</td><td class="align_center">0.05</td></tr><tr><td class="align_left">Mode 2</td><td class="align_center">1.2761</td><td class="align_center">0.06</td></tr><tr><td class="align_left">Mode 3</td><td class="align_center">1.6538</td><td class="align_center">0.08</td></tr><tr><td class="align_left">Mode 4</td><td class="align_center">2.2893</td><td class="align_center">0.025</td></tr><tr class="table-tr"><td colspan="3"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>Parameters of the flexible dynamics.</div>

Shock and Vibration

tab1

Table 1

Table 1: Attitude Maneuvering and Vibration Reducing Control of Flexible Spacecraft Subject to Actuator Saturation and Misalignment 