Ir. Yvonne Ferrier

Ir. Yvonne Ferrier

MSc 2016-2017

This thesis focuses on designing an active gust load alleviation control law for aircraft with flexible wings. The control law is verified on the NASA Generic Transport Model (GTM). Link to the thesis.

This project leads to a publication in the AIAA SciTech 2018, Guidance, Navigation, and Control Conference. Link to the paper.


  • Active Gust Load Alleviation for Flexible Wing Aircraft