Adaptive and Resilient Flight Control System for a Small Unmanned Aerial System

<table><svg height="12.675" id="M318" style="vertical-align:-0.0pt" version="1.1" viewbox="0 0 13.4625 12.675" width="13.4625" xmlns="http://www.w3.org/2000/svg" xmlns:xlink="http://www.w3.org/1999/xlink">
<g transform="matrix(.017,-0,0,-.017,.625,12.05)"><path d="M698 636l-541 -596q60 -5 176 -5q91 0 138.5 5t69.5 24q44 36 85 124l29 -15q-38 -125 -64 -173h-559l-9 16l545 598h-182q-81 0 -109 -8t-48 -31q-26 -29 -55 -103l-29 3q23 86 42 200h22q11 -16 21 -20.5t34 -4.5h428z" id="x1D44D"></path></g>
</svg>-axis measured and predicted acceleration: larger flight portion (a); zoom after switching control (b).</table>

International Journal of Aerospace Engineering

fig12

Figure 12

Figure 12: Adaptive and Resilient Flight Control System for a Small Unmanned Aerial System 