| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 4974364 | Journal of the Franklin Institute | 2017 | 17 Pages |
Abstract
A new synthesis procedure is introduced for static Hâ loop shaping problem in discrete-time case. LMI conditions are derived to obtain a static output feedback controller that ensures the robust stability and performance of the closed-loop system. A numerical example illustrates the use of the proposed control method with application to a VTOL (“vertical take-off landing”) aircraft model.
Related Topics
Physical Sciences and Engineering
Computer Science
Signal Processing
Authors
Renan L. Pereira, Karl H. Kienitz, Fernando H.D. Guaracy,