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Application of Microprocessors to Aircraft Fly-By-Wire Hydraulic Actuation Systems, SAE Committee A-6 1983
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English
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.
Authors
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, https://doi.org/10.4271/831489.Also In
References
- Boeing Commercial Airplane Company “Integrated Application of Active Controls (IAAC) Technology to an Advanced Subsonic Transport Project--Initial ACT Configuration Design Study” NASA Contractor Report 159249 July 1980
- Krogh S. B. “Specification for Digital Integrated Servoactuator Controller (DISAC) for Reconfigurable Fly-by-Wire Actuation System” Boeing Document D180-26981-1 May 1982
- Krogh S. B. “Specification for Actuator Control Computer (ACC) for Reconfigurable Fly-by-Wire Actuation System” Boeing Document D180-26849-1 May 1982