A modular electronic control system is disclosed. The modular electronic control system may have a base control unit to which one or more internal subsystem module and/or external subsystem module may be mounted. Each subsystem module may perform a different function, or may connect with different sensors/effectors, however, each subsystem module has a standardized subsystem module mounting apparatus by which it can mechanically and electrically connect to the base control unit. As such, a standardized base control unit may receive any type of internal subsystem module and/or external subsystem module and intermediate communication and power provision between subsystem module and other aircraft systems, such as an aircraft data network.


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    Title :

    Electronic Control with Interchangeable Subsystem Modules


    Contributors:

    Publication date :

    2016-08-18


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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