Aircraft display and control system with virtual backplane archi

Boots – shoes – and leggings

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Details

395280, 395282, 395309, 36442406, G06F 1300

Patent

active

057782032

ABSTRACT:
An aircraft control system improves system flexibility, scalability, redundancy, and separation. The system uses a "virtual backplane" architecture which maximizes system flexibility and scalability and allows easy integration of new functions. The architecture comprises four major elements: processing modules; input and output modules (i.e. I/O modules); database modules; and an aircraft wide system network. Inter module communication occurs via the aircraft wide system network thereby eliminating the need for point to point communication and making modules independent of physical location or what modular units (MUs) they are in. Predetermined periodic and deterministic broadcast techniques improve the safety and communications efficiency of the system.

REFERENCES:
patent: 5412651 (1995-05-01), Gorshe
patent: 5426774 (1995-06-01), Banerjee et al.
patent: 5544329 (1996-08-01), Engel et al.

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