Errata: C matrix in Example 8.7 (vectored thrust aircraft) is incorrect

Chapter	Output Feedback
Page	8-21
Line	4
Version	3.1.5
Date	5 May 2024

The output matrix $C$ in Example 8.7 is incorrect. It should correspond to the $x$ position of the aircraft:

$C={\begin{bmatrix}1&0&0&0\end{bmatrix}}.$