A simple model to simulate the lateral motion during the takeoff of an aerodynamically unstable aircraft is presented. By neglecting the landing gear dynamics no additional solution of the corresponding differential equations was required. Landing gear forces were determined from the geometrical ratios of the aircraft to the ground reference line. This procedure is particularly efficient when no high frequency landing gear drive-as, e.g., during touchdown has to be taken into account. The objection free function of the control concept for an aircraft aerodynamically unstable in the lateral plane is shown.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Description of a Simple Model to Determine Landing Gear Forces During the Takeoff of Aerodynamically Unstable Aircraft Beschreibung Eines Einfachen Modells Zur Ermittlung von Fahrwerkskraeften Waehrend des Startvorgangs Eines Aerodynamisches Instabilen Flugzeugs


    Beteiligte:
    M. Soelter (Autor:in)

    Erscheinungsdatum :

    1981


    Format / Umfang :

    43 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch






    Verfahren zur Ermittlung der Luftgeschwindigkeit eines Flugzeugs

    STEINGASS ALEXANDER | Europäisches Patentamt | 2018

    Freier Zugriff


    Temperaturüberwachung eines Flugzeugs

    PAUTSCH CHRISTIAN / WOHLERS WOLFGANG | Europäisches Patentamt | 2017

    Freier Zugriff