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Fault tolerant control for partial loss of control authority in aircraft using piecewise affine slab models


Fault tolerant control for partial loss of control authority in aircraft using piecewise affine slab models

Nayebpanah, Nastaran, Rodrigues, Luis and Zhang, Youmin (2013) Fault tolerant control for partial loss of control authority in aircraft using piecewise affine slab models. Journal of the Franklin Institute . ISSN 00160032 (In Press)

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rodrigues2013.pdf - Accepted Version

Official URL: http://dx.doi.org/10.1016/j.jfranklin.2013.02.023


In this paper, a new fault tolerant control methodology is proposed for partial loss of control authority in aircraft using piecewise affine (PWA) slab models while minimizing an upper bound on a quadratic cost function. The proposed controller stabilizes and satisfies performance bounds for both the nominal and faulty systems. The controller design criteria are cast as a set of Linear Matrix Inequalities (LMIs) that can be solved efficiently. The new technique is illustrated in a numerical example for the Beechcraft 99 aircraft model.

Divisions:Concordia University > Gina Cody School of Engineering and Computer Science > Electrical and Computer Engineering
Item Type:Article
Authors:Nayebpanah, Nastaran and Rodrigues, Luis and Zhang, Youmin
Journal or Publication:Journal of the Franklin Institute
Digital Object Identifier (DOI):10.1016/j.jfranklin.2013.02.023
ID Code:977031
Deposited On:08 Apr 2013 14:21
Last Modified:18 Jan 2018 17:43


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