A method for integrating a constrained aircraft route(s) optimization application is implemented in an avionics onboard system comprising a DAL+ core computer and a DAL− peripheral computer for managing the application. The method of integration determines an optimal functional and physical distribution of the elementary functions OPT_RTE_FU(i) of the application within the onboard avionics system over the set of possible distributions which minimizes a global cost criterion CG, dependent on several parameters, including at least the additional development cost of the elementary functions integrated within the DAL+ digital core computer, and carries out the integration of the application.


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    Titel :

    PROCEDE D'INTEGRATION D'UNE APPLICATION D'OPTIMISATION DE ROUTE (S) SOUS CONTRAINTES DANS UN SYSTEME EMBARQUE AVIONIQUE A ARCHITECTURE OUVERTE DE TYPE CLIENT SERVEUR


    Beteiligte:
    NEFFLIER FRANCOIS (Autor:in) / AULFINGER HERVE (Autor:in) / PIERRE PATRICK (Autor:in)

    Erscheinungsdatum :

    11.05.2018


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Französisch


    Klassifikation :

    IPC:    G01C Messen von Entfernungen, Höhen, Neigungen oder Richtungen , MEASURING DISTANCES, LEVELS OR BEARINGS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G06F ELECTRIC DIGITAL DATA PROCESSING , Elektrische digitale Datenverarbeitung