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Cited article:

A linear parameter-varying multiobjective control law design based on youla parametrization for a flexible blended wing body aircraft

F. Demourant, G. Ferreres

Published online: 2013-12-02

DOI: https://doi.org/10.1051/eucass/201306729

This article has been cited by the following article(s):

Gust Load Alleviation: Identification, Control, and Wind Tunnel Testing of a 2-D Aeroelastic Airfoil

Charles Poussot-Vassal, Fabrice Demourant, Arnaud Lepage and Dominique Le Bihan
IEEE Transactions on Control Systems Technology 25 (5) 1736 (2017)
https://doi.org/10.1109/TCST.2016.2630505

Modeling and Control for a Blended Wing Body Aircraft

A. Schirrer, M. Kozek, F. Demourant and G. Ferreres
Advances in Industrial Control, Modeling and Control for a Blended Wing Body Aircraft 147 (2015)
https://doi.org/10.1007/978-3-319-10792-9_6