Correction to: Flight-Test Plan Design and Evaluation in a Closed-Loop Framework for a General Aviation Aircraft (AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022)

Correction Notice For figure 21, which describes the flight envelope of the underlying aircraft model, wrong figure files were unfortunately used. Please find the correct figures for the investigated aircraft below. This change does not affect the published results, but strongly influences the interpretation of the underlying aircraft model (and also of the results). Moreover, in equation 33 the term (formula presented) is missing, indicating a possible error in the published results due to a wrong model formulation. Since the used linear model, that is described by equation 33, is obtained programmatically (based on trimming and linearization) the error in the published model formulation does not affect the results. This simple error should however be addressed, since it can lead to misinterpretation of the published results. Please find the correct model structure below (equation 33).