dc.creator | Koumboulis, F. N. | en |
dc.creator | Skarpetis, M. G. | en |
dc.date.accessioned | 2015-11-23T10:36:08Z | |
dc.date.available | 2015-11-23T10:36:08Z | |
dc.date.issued | 1996 | |
dc.identifier | 10.1049/ip-cta:19960301 | |
dc.identifier.issn | 1350-2379 | |
dc.identifier.uri | http://hdl.handle.net/11615/29803 | |
dc.description.abstract | For a test aircraft in a wind tunnel with magnetic suspension and balance systems, a decoupling control configuration is proposed. Using the input-output decoupling technique the flight variables are controlled independently at all frequencies and for all aerodynamic and electromagnetic conditions. The decoupling controllers are static. The performance of the resulting closed-loop system is quite satisfactory. | en |
dc.source | Iee Proceedings-Control Theory and Applications | en |
dc.source.uri | <Go to ISI>://WOS:A1996VC81700006 | |
dc.subject | magnetic suspension | en |
dc.subject | decoupled closed-loop system | en |
dc.subject | wind tunnel | en |
dc.subject | LINEAR-MULTIVARIABLE SYSTEMS | en |
dc.subject | Automation & Control Systems | en |
dc.subject | Engineering, Electrical & Electronic | en |
dc.subject | Instruments & Instrumentation | en |
dc.title | Static controllers for magnetic suspension and balance systems | en |
dc.type | journalArticle | en |