@inproceedings{13eed8c8feed414184943d7c25a50ff3,
title = "Structural model identification of a small flexible aircraft",
abstract = "The system identification of a light-weight, high-aspect ratio wing is presented. Experimental data is obtained from a ground vibration test. The input signals are sine sweep wave forces and the outputs are the corresponding acceleration responses of the aircraft. Subspace algorithms are used to estimate a state-space model of the aircraft. Minimization of the model prediction error is performed to fit the frequency response data. As result, the estimated model identifies six structural modes between 5 Hz and 30 Hz.",
keywords = "Flexible structures, Identification, Linear systems",
author = "Moreno, {Claudia P.} and Abhineet Gupta and Harald Pfifer and Brian Taylor and Balas, {Gary J.}",
note = "Copyright: Copyright 2014 Elsevier B.V., All rights reserved.; 2014 American Control Conference, ACC 2014 ; Conference date: 04-06-2014 Through 06-06-2014",
year = "2014",
doi = "10.1109/ACC.2014.6859471",
language = "English (US)",
isbn = "9781479932726",
series = "Proceedings of the American Control Conference",
publisher = "Institute of Electrical and Electronics Engineers Inc.",
pages = "4379--4384",
booktitle = "2014 American Control Conference, ACC 2014",
}