A distributed controller of an aircraft includes a first communication device, a second communication device, and at least one processor. The first communication device is configured to transmit heater status data and receive heater command data via radio waves or power-line communication. The second communication device is configured to transmit at least one heater control signal and to receive heater sensor data. The at least one processor is configured to provide heater control based upon the heater command data and the heater sensor data and to provide heater status information based upon the received heater sensor data.
REDUCED-WIRING CONTROLLER FOR AIRCRAFT USE
2019-08-15
Patent
Elektronische Ressource
Englisch
Tema Archiv | 1968
Engineering Index Backfile | 1945
|Engineering Index Backfile | 1944
|Engineering Index Backfile | 1945
|Engineering Index Backfile | 1944
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