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 languageUndefined
    Title of host publicationProceedings of the 15th IFAC World Congress
    EditorsE.F. Camacho, L. Basanez, J.A. de la Puente
    Place of PublicationAmsterdam
    PublisherElsevier
    Pages49-53
    Number of pages6
    ISBN (Print)978-0-08-044295-2
    Publication statusPublished - 2002
    Event15th IFAC World Congress 2002 - Barcelona, Spain
    Duration: 21 Jul 200226 Jul 2002
    Conference number: 15
    http://folk.ntnu.no/skoge/prost/proceedings/ifac2002/home.htm

    Publication series

    Name
    PublisherElsevier

    Conference

    Conference15th IFAC World Congress 2002
    CountrySpain
    CityBarcelona
    Period21/07/0226/07/02
    Internet address

    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.