A computer implemented method for integrating a platform, different stores, and/or carriage racks is implemented in an electronics control system that is communicatively couplable to each of the platform, the different stores, and/or the carriage racks. The computer implemented method includes defining parameters for a plurality of predetermined electrical interfaces for predetermined platforms, stores, and carriage racks, and message sets corresponding thereto, identifying electrical interfaces of the platform, at least one store and/or at least one carriage rack based on the defined parameters, communicating different messages between the platform, the store and/or the carriage rack without affecting an Operational Flight Program (OFP) of the platform, with each communication between the platform, and the store and/or the carriage rack being independent, translating messages between the platform and the store and/or the carriage rack, and controlling operation of the carriage rack and/or the store based on the messages.


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    Title :

    AIRCRAFT ARMAMENT SYSTEM CONTROL ELECTRONICS


    Contributors:

    Publication date :

    2021-03-04


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F41G Zielvorrichtungen für Waffen , WEAPON SIGHTS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    AIRCRAFT ARMAMENT SYSTEM CONTROL ELECTRONICS

    FEATHERSTON KATHERINE / BROADHEAD DAVID J / DEININGER GREGORY J | European Patent Office | 2020

    Free access

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