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Analysis Of The Method Of Predictive Control Applicable To Active Magnetic Suspension Systems Of Aircraft Engines

Paulina Kurnyta-Mazurek / Maciej Henzel / Artur Kurnyta
Published Online: 2016-01-06 | DOI: https://doi.org/10.1515/afit-2015-0034


Conventional controllers are usually synthesized on the basis of already known parameters associated with the model developed for the object to be controlled. However, sometimes it proves extremely difficult or even infeasible to find out these parameters, in particular when they subject to changes during the exploitation lifetime. If so, much more sophisticated control methods have to be applied, e.g. the method of predictive control. Thus, the paper deals with application of the predictive control approach to follow-up tracking of an active magnetic suspension where the mathematical and simulation models for such a control system are disclosed with preliminary results from simulation investigations of the control system in question.

Keywords: active magnetic suspension; predictive control method; follow-up adaptive control method


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About the article

Published Online: 2016-01-06

Published in Print: 2015-12-01

Citation Information: Research Works of Air Force Institute of Technology, Volume 37, Issue 1, Pages 195–205, ISSN (Online) 2083-8573, ISSN (Print) 1234-3544, DOI: https://doi.org/10.1515/afit-2015-0034.

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© 2015 Wydawnictwo Instytutu Technicznego Wojsk Lotniczych. This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 3.0 License. BY-NC-ND 3.0

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