Publisher DOI: 10.1016/S0967-0661(98)00190-7
Title: Robust control of a laboratory aircraft model via fast output sampling
Language: English
Authors: Werner, Herbert 
Meister, Tilo 
Keywords: Linear matrix inequalities; Measurement noise; Multirate; Output feedback; Robust control; Sampled-data control; State feedback; Trade-offs
Issue Date: 30-Apr-1999
Publisher: Elsevier Science
Source: Control Engineering Practice 7 (3): 305-313 (1999)
Abstract (english): 
A new multimodel approach to robust controller design is illustrated by a practical application: for a laboratory aircraft model, a robust controller is designed for acceptable performance, in normal operating conditions and under propeller failure, simultaneously. Based on a linear model for each operating mode, linear matrix inequality (LMI) formulation of the problem and convex programming are used to search for a state feedback controller that achieves the objective. This state feedback design is then realized simultaneously in both operating modes by a controller that is based on fast output sampling. Robust performance is demonstrated by experimental results. © 1999 Elsevier Science Ltd. All rights reserved.
ISSN: 0967-0661
Journal: Control engineering practice 
Document Type: Article
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