Actuator and Sensor Positioning Optimization in Control Design for a Large BWB Passenger Aircraft

<table>Illustration of the utilized BWB aircraft model with one modeled control surface (spanwise length <svg height="11.84125" id="M138" style="vertical-align:-0.1254pt" version="1.1" viewbox="0 0 6.2150002 11.84125" width="6.2150002" xmlns="http://www.w3.org/2000/svg">
<g transform="matrix(1.25,0,0,-1.25,0,11.84125)">
<text transform="matrix(1,0,0,-1,0.498,0.623)">
<tspan style="font-size: 12.50px; " x="0" y="0">𝑙</tspan>
</text>
</g>
</svg>, center <svg height="10.9825" id="M139" style="vertical-align:-2.29482pt" version="1.1" viewbox="0 0 8.9975004 10.9825" width="8.9975004" xmlns="http://www.w3.org/2000/svg">
<g transform="matrix(1.25,0,0,-1.25,0,10.9825)">
<text transform="matrix(1,0,0,-1,0.498,2.786)">
<tspan style="font-size: 12.50px; " x="0" y="0">𝑦</tspan>
</text>
</g>
</svg>-coordinate <svg height="15.7025" id="M140" style="vertical-align:-3.22281pt" version="1.1" viewbox="0 0 11.71375 15.7025" width="11.71375" xmlns="http://www.w3.org/2000/svg">
<g transform="matrix(1.25,0,0,-1.25,0,15.7025)">
<text transform="matrix(1,0,0,-1,0.498,3.711)">
<tspan style="font-size: 12.50px; " x="0" y="0">𝑙</tspan>
</text>
<text transform="matrix(1,0,0,-1,4.474,0.586)">
<tspan style="font-size: 8.75px; " x="0" y="0">c</tspan>
</text>
</g>
</svg>).</table>

International Scholarly Research Notices

fig4

Figure 4

Figure 4: Actuator and Sensor Positioning Optimization in Control Design for a Large BWB Passenger Aircraft 