An investigation into the applicability of fiber optic communication techniques to real time avionic control systems, in particular the total automatic flight control system used for the VSTOL aircraft is presented. The system consists of spatially distributed microprocessors. The overall control function is partitioned to yield a unidirectional data flow between the processing elements (PE). System reliability is enhanced by the use of triple redundancy. Some general overall system specifications are listed here to provide the necessary background for the requirements of the communications system.
Intercommunications in Real Time, Redundant, Distributed Computer System
1980
57 pages
Report
Keine Angabe
Englisch
Vehicular Intercommunications System
NTIS | 1978
|Vehicular Intercommunications System
NTIS | 1980
|Vehicular Intercommunications System
NTIS | 1978
|Vehicular Intercommunications Systems
NTIS | 1979
|