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MIXED SENSITIVITY DESIGN: AN AEROSPACE CASE STUDY
Huibert Kwakernaak
Systems, Signals and Control, Faculty of Mathematical Sciences, University of Twente
P.O. Box 217, 7500 AE Enschede, The Netherlands
E-mail h.kwakernaak@math.utwente.nl
The mixed sensitivity design method for multivariable linear control systems proposed in the companion paper (Kwakernaak, submitted for B02) is applied to the design of a stability augmentation system for the longitudinal motion of a fighter airplane previously studied by Safonov and Chiang (1988). Both H∞ and H2 mixed sensitivity designs are considered. They lead to quite similar results
Keywords: Mixed sensitivity design, stability augmentation system, H∞ optimization, H2 optimization
Session slot T-Tu-M06: Recent MIMO Design Approaches for Aerospace Application/Area code 8a : Aerospace
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