Vibration Reduction Design and Test of UAV Load Radar

<table class="table-group" id="tab1"><tr><td><table class="table"><tr><td class="thead-hr" colspan="6"><hr/></td></tr><tr class="thead"><td class="align_left">Label</td><td class="align_center">D1</td><td class="align_center">D2</td><td class="align_center">L1</td><td class="align_center">L2</td><td class="align_center">L3</td></tr><tr><td class="thead-hr" colspan="6"><hr/></td></tr><tr><td class="align_left">Value (mm)</td><td class="align_center">20</td><td class="align_center">8</td><td class="align_center">30</td><td class="align_center">8.5</td><td class="align_center">12.3</td></tr><tr class="table-tr"><td colspan="6"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>Main dimensions of T-type rubber isolator.</div>

International Journal of Aerospace Engineering

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Table 1

Table 1: Vibration Reduction Design and Test of UAV Load Radar 