Application of Microprocessors to Aircraft Fly-By-Wire Hydraulic Actuation Systems, SAE Committee A-6 1983
Date Published: 1983-10-03
Paper Number:831489
DOI: 10.4271/831489
Citation:
Krogh, S. and Chenoweth, C., "Application of Microprocessors to Aircraft Fly-By-Wire Hydraulic Actuation Systems, SAE Committee A-6 1983," SAE Technical Paper 831489, 1983, doi:10.4271/831489.
Author(s):
S. B. Krogh - Flight Controls Technology Boeing Military Airplane Co.
C. C. Chenoweth - Flight Controls Technology Boeing Military Airplane Co.
Abstract:
Actuation systems have been slow to take advantage of advancements in electronics and computer technology, now prevalent in other parts of advanced flight control systems. Two types of microprocessor-based actuator controllers are being developed which utilize these advancements. These controllers will allow the implementation of advanced reliable Fly-by-wire flight control systems which are compatible with distributed processing techniques. Benefits include reduced cost and weight, improved survivability and enhanced test and functional capability.
File Size: 267K
Product Status: In Stock
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