The Lockheed L-1011 automatic flight control systems - yaw stability augmentation and automatic landing - are described in terms of their redundancies. The reliability objectives for these systems are discussed and related to in-service experience. In general, the availability of the stability augmentation system is higher than the original design requirement, but is commensurate with early estimates. The in-service experience with automatic landing is not sufficient to provide verification of Category 3 automatic landing system estimated availability.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Lockheed L-1101 avionic flight control redundant systems


    Beteiligte:


    Erscheinungsdatum :

    1976-08-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Tornado avionic flight testing

    PEARSON, E. | AIAA | 1986



    No. 1101

    DataCite | 1926


    Nr. 1101

    DataCite | 1866

    Freier Zugriff