Mixed sensitivity design: An aerospace case study

H. Kwakernaak

Research output: Chapter in Book/Report/Conference proceedingConference contributionProfessional

3 Citations (Scopus)

Abstract

The mixed sensitivity design method for multivariable linear control systems proposed in the companion paper (Kwakernaak, 2001) 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 $H_\infty$ and $H_2$ mixed sensitivity design are considered. They lead to quite similar results
Original language Undefined Proceedings of the 15th IFAC World Congress E.F. Camacho, L. Basanez, J.A. de la Puente Amsterdam Elsevier 49-53 6 978-0-08-044295-2 Published - 2002 15th IFAC World Congress 2002 - Barcelona, SpainDuration: 21 Jul 2002 → 26 Jul 2002Conference number: 15http://folk.ntnu.no/skoge/prost/proceedings/ifac2002/home.htm

Publication series

Name Elsevier

Conference

Conference 15th IFAC World Congress 2002 Spain Barcelona 21/07/02 → 26/07/02 http://folk.ntnu.no/skoge/prost/proceedings/ifac2002/home.htm

Keywords

• METIS-211772
• IR-69135
• EWI-16733

Cite this

Kwakernaak, H. (2002). Mixed sensitivity design: An aerospace case study. In E. F. Camacho, L. Basanez, & J. A. de la Puente (Eds.), Proceedings of the 15th IFAC World Congress (pp. 49-53). Amsterdam: Elsevier.