“The Impact Of The Microprocessor On Aircraft Electric System Control Philosophy”

811085

10/01/1981

Authors
Abstract
Content
The use of microprocessors for the implementation of control functions in aircraft electric systems has become a reality. This paper presents a brief survey of these systems along with a typical system block diagram. A description of the diagram highlights the advantages of microprocessor systems over existing noncomputerized control schemes.
The second half of the paper discusses the adaptability of more advanced microprocessor systems in the next generation of aircraft electric systems. These powerful new computers will allow digital control and protection of single unit and paralleled generating and starting systems, as well as providing even more effective built-in-test.
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DOI
https://doi.org/10.4271/811085
Pages
12
Citation
Ruffner, B., "“The Impact Of The Microprocessor On Aircraft Electric System Control Philosophy”," SAE Technical Paper 811085, 1981, https://doi.org/10.4271/811085.
Additional Details
Publisher
Published
Oct 1, 1981
Product Code
811085
Content Type
Technical Paper
Language
English