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.
Electronic Control with Interchangeable Subsystem Modules
18.08.2016
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |