Disclosed is an apparatus of setting a dimension parameter relating to a value of a shock absorber dimension of a shock absorber of an aircraft landing gear, the shock absorber dimension being indicative of an extension of the shock absorber. The apparatus comprises a processor configured to identify a respective range of values relating to each of a plurality of operating characteristics under which the shock absorber may operate, and identify a respective probability distribution of values for each of the operating characteristics within the identified ranges. The processor is also configured to perform a generation process for generating a plurality of values of the shock absorber dimension by repeatedly selecting, as input into a computer-implemented model for determining a value of the shock absorber dimension, a value of each of the operating characteristics based on the respective probability distributions, and determining a given value of the shock absorber dimension using the selected values and the computer-implemented model. The processor is also configured to set the dimension parameter based on the generated plurality of shock absorber dimension values.


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    Title :

    SHOCK ABSORBER DIMENSION


    Additional title:

    STOSSDÄMPFERABMESSUNG
    DIMENSION D'ABSORBEUR DE CHOCS


    Contributors:

    Publication date :

    2018-11-21


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    G06F ELECTRIC DIGITAL DATA PROCESSING , Elektrische digitale Datenverarbeitung / B64C AEROPLANES , Flugzeuge



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