The European Fighter Aircraft (EFA) was designed as a highly augmented, basically unstable aircraft. Its Stability and Control System (FCS) is of a much higher complexity than that used in earlier aircraft, e.g., the Tornado. To ensure that safe operation and optimum performance are not degraded due to possible handling quality deficiencies, new methods had to be used for both the development and the assessment of the aircraft. This paper describes the specifications and the methods used in customer assessment prior to first flight. An overview of these methods is provided.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    EFA Flying Qualities Specification and Its Utilisation


    Beteiligte:
    M. Marchand (Autor:in) / R. Koehler (Autor:in) / H. Duda (Autor:in) / E. Buchacker (Autor:in) / K. Elbel (Autor:in)

    Erscheinungsdatum :

    1994


    Format / Umfang :

    18 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    EFA Flying Qualities Specification and its Utilisation

    Marchand, M. / Kochler, R. / Duda, H. et al. | British Library Conference Proceedings | 1994



    Airplane flying qualities specification revision

    CHALK, C. / WILSON, R. | AIAA | 1968


    Perspectives of the flying qualities specification

    FULLER, S. / MOORHOUSE, D. | AIAA | 1982