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. |
URI: | http://hdl.handle.net/11420/14709 | ISSN: | 0967-0661 | Journal: | Control engineering practice | Document Type: | Article |
Appears in Collections: | Publications without fulltext |
Show full item record
Add Files to Item
Note about this record
Cite this record
Export
Items in TORE are protected by copyright, with all rights reserved, unless otherwise indicated.