Tendon-Sheath Mechanisms in Flexible Membrane Wing Mini-UAVs: Control and Performance

<table class="table-group" id="tab1"><tr><td><table class="table"><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr><td class="align_left">Wingspan</td><td class="align_center">1 m</td></tr><tr><td class="align_left">Chord length</td><td class="align_center">0.25 m</td></tr><tr><td class="align_left">Mean aerodynamic chord</td><td class="align_center">0.22 m</td></tr><tr><td class="align_left">Area</td><td class="align_center">0.19 m<sup>2</sup></td></tr><tr><td class="align_left">Aspect ratio</td><td class="align_center">5.158</td></tr><tr><td class="align_left">Weight</td><td class="align_center">160 g</td></tr><tr class="table-tr"><td colspan="2"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

International Journal of Aerospace Engineering

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Table 1

Table 1: Tendon-Sheath Mechanisms in Flexible Membrane Wing Mini-UAVs: Control and Performance 