A controller unit for an aircraft control system includes an interface that is electrically connectable to a controller slot of an electronics bay of the aircraft control system, a processor coupled to the interface, and a tangible non-transitory computer-readable medium having instructions stored thereon that, in response to execution by the processor, cause the processor to perform various operations. The various operations include identifying, by the processor, a first aircraft assembly in electrical communication with the controller slot of the electronics bay, identifying, by the processor, a first program code stored on the tangible non-transitory computer-readable medium corresponding to the first aircraft assembly, and selecting, by the processor, the first program code to control the first aircraft assembly.
AIRCRAFT CONTROL SYSTEM ARCHITECTURE
19.04.2018
Patent
Elektronische Ressource
Englisch
Aircraft electrical brake control system architecture
Europäisches Patentamt | 2017
|Aircraft electrical brake control system architecture
Europäisches Patentamt | 2017
|AIRCRAFT OPERATING METHOD, AIRCRAFT CONTROL PANEL ARCHITECTURE, AND AIRCRAFT
Europäisches Patentamt | 2024
|AIRCRAFT OPERATING METHOD, AIRCRAFT CONTROL PANEL ARCHITECTURE, AND AIRCRAFT
Europäisches Patentamt | 2022
|