A system for determining a deceleration rate of an aircraft, in various embodiments, includes at least one component capable of transmitting a first deceleration rate. The system also includes a brake control unit coupled to the at least one component and having a brake controller that is configured to receive the first deceleration rate from the at least one component and to determine a likely accurate deceleration rate based on the first deceleration rate, a second deceleration rate and a hierarchy of sources of deceleration rates.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Robustness and availability of aircraft acceleration evaluation


    Beteiligte:
    GEORGIN MARC (Autor:in)

    Erscheinungsdatum :

    2019-05-21


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B60T Bremsanlagen für Fahrzeuge oder Teile davon , VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    ROBUSTNESS AND AVAILABILITY OF AIRCRAFT ACCELERATION EVALUATION

    GEORGIN MARC | Europäisches Patentamt | 2017

    Freier Zugriff

    IMPROVED ROBUSTNESS AND AVAILABILITY OF AIRCRAFT ACCELERATION EVALUATION

    GEORGIN MARC | Europäisches Patentamt | 2020

    Freier Zugriff



    Predicting Aircraft Availability

    M. A. Chapa | NTIS | 2013