A controller for an electrohydraulic active control landing gear was developed for the F-4 aircraft. A controller was modified for this application. Simulation results indicate that during landing and rollout over repaired bomb craters the active gear effects a force reduction, relative to the passive gear, or approximately 70%.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    An electronic control for an electrohydraulic active control landing gear for the F-4 aircraft


    Beteiligte:
    Ross, I. (Autor:in)

    Erscheinungsdatum :

    1982-04-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





    AIRCRAFT LANDING GEAR CONTROL SYSTEM

    SANADIKI M NIZAR | Europäisches Patentamt | 2024

    Freier Zugriff



    Fuzzy Control of Aircraft Semi-active Landing Gear System

    Wang, X. / Carl, U. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 1999