Title: The implementation of fail-operative functions in integrated digital avionics systems
Abstract: System architectures which incorporate fail operative flight guidance functions within a total integrated avionics complex are described. It is shown that the mixture of flight critical and nonflight critical functions within a common computer complex is an efficient solution to the integration of navigation, guidance, flight control, display, and flight management. Interfacing subsystems retain autonomous capability to avoid vulnerability to total avionics system shutdown as a result of only a few failures.
Publication Year: 1976
Publication Date: 1976-08-01
Language: en
Type: article
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