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Static controllers for magnetic suspension and balance systems

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2 Author(s)
Koumboulis, F.N. ; Sch. of Technol. Sci., Thessaly Univ., Volos, Greece ; Skarpetis, M.G.

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

Published in:

Control Theory and Applications, IEE Proceedings -  (Volume:143 ,  Issue: 4 )