A method 200 and apparatus for selecting aircraft system components comprising providing a reliability evaluation function 202 that produces a reliability score for a given set of candidate components for the aircraft system, and a complexity evaluation function 204 that produces a complexity score representative of a complexity of installing a given set of candidate components for the aircraft system. A multi-objective optimisation function 206 is performed to determine at least one set of candidate components for the system that satisfy one or more conditions relating to at least one of the produced scores, wherein the optimisation function iteratively selects 208 a new set of candidate components for the system, performs at least one of the reliability or complexity functions to generate a reliability score and/or complexity score 210 for the candidate components, and evaluates at least one of these scores according to one of the conditions 212 for storing 214 the components based on the evaluation.


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    Title :

    Aircraft component selection


    Contributors:

    Publication date :

    2024-01-31


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    G06Q Datenverarbeitungssysteme oder -verfahren, besonders angepasst an verwaltungstechnische, geschäftliche, finanzielle oder betriebswirtschaftliche Zwecke, sowie an geschäftsbezogene Überwachungs- oder Voraussagezwecke , DATA PROCESSING SYSTEMS OR METHODS, SPECIALLY ADAPTED FOR ADMINISTRATIVE, COMMERCIAL, FINANCIAL, MANAGERIAL, SUPERVISORY OR FORECASTING PURPOSES / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



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