@inproceedings{b6aef36351f84fdcadd1c7d4846404a8,
title = "Adaptive linear quadratic gaussian optimal control modification for flutter suppression of adaptive wing",
abstract = "This paper presents an adaptive control approach for flutter suppression control of a performance adaptive aeroelastic wing equipped with a variable camber continuous trailing edge flap design. The adaptive control approach is based on the optimal control modification method augmented to a linear quadratic gaussian optimal control design. A model reduction based on a singular perturbation approach is presented. The control surfaces are subject to relative motion constraints due to the elastomer transition material in between the flap sections. A virtual control method is proposed using a shape function to deal with the relative motion constraints. Simulation results indicate that the adaptive augmentation control design is effective in suppressing unstable aeroelastic modes.",
author = "Nguyen, {Nhan T.} and Sean Swei and Eric Ting",
note = "Publisher Copyright: {\textcopyright} 2015, American Institute of Aeronautics and Astronautics Inc. All rights received.; AIAA Infotech @ Aerospace 2015 ; Conference date: 05-01-2015 Through 09-01-2015",
year = "2015",
doi = "10.2514/6.2015-0118",
language = "British English",
series = "AIAA Infotech at Aerospace",
booktitle = "AIAA Infotech at Aerospace",
}