Research on Microvibrations Generated by a Control Moment Gyroscope on a Flexible Interface Based on a Dynamic Substructure Method

<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">Young’s modulus (<i>E</i>)</td><td class="align_center">Density (<i>ρ</i>)</td><td class="align_center">Poisson ratio (<i>υ</i>)</td></tr><tr><td class="thead-hr" colspan="3"><hr/></td></tr><tr><td class="align_left">71 GPa</td><td class="align_center">2700 kg/m<sup>3</sup></td><td class="align_center">0.33</td></tr><tr class="table-tr"><td colspan="3"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>Material properties of the aluminum alloy.</div>

International Journal of Aerospace Engineering

tab1

Table 1

Table 1: Research on Microvibrations Generated by a Control Moment Gyroscope on a Flexible Interface Based on a Dynamic Substructure Method 