@inproceedings{a460354ae8bd4077a81df177497d956e,
title = "Reliable Aircraft Flight Control Using Static Output-Feedback",
abstract = "In this paper, aircraft model with control surface impairment faults is described as a set of affine parameter-dependent linear systems. New tests for stability and performance for this type of systems are presented. Based on these tests, a reliable tracking controller design method via static output feedback is given. These tests and design method are based on the notion of affine quadratic stability/performance and solvability of linear matrix inequalities (LMIs), and have less conserv-ativeness than existing methods. Design and simulation results are presented to illustrate the advantage of the proposed approach over standard flight controllers.",
keywords = "Affine quadratic stability/performance test, Control surface impairment, LMI, Reliable aircraft control, Static output feedback, Tracking",
author = "Fang Liao and Wang, {Jian Liang} and Yang, {Guang Hong}",
year = "2002",
language = "English",
isbn = "9781563479786",
series = "AIAA Guidance, Navigation, and Control Conference and Exhibit",
publisher = "AIAA International",
booktitle = "AIAA Guidance, Navigation, and Control Conference and Exhibit",
address = "United States",
note = "AIAA Guidance, Navigation, and Control Conference and Exhibit 2002 ; Conference date: 05-08-2002 Through 08-08-2002",
}