FULL AUTHORITY FAULT TOLERANT ELECTRONIC ENGINE CONTROL SYSTEMS FOR ADVANCED HIGH PERFORMANCE ENGINES (FAFTEEC)

821398

02/01/1982

Event
Aerospace Congress and Exposition
Authors Abstract
Content
Over the past three decades gas turbine engine technology for high performance, multi-mission aircraft has progressed from hydromechanical designs to full authority digital electronic control systems. Future weapon systems will require propulsion controls that are highly integrated with the flight control, and since the engine control then becomes part of the flight control system, safety will require fault tolerant capabilities. Realizing this, the Air Force sponsored the Full Authority Fault Tolerant Electronic Engine Control (FAFTEEC) Program1 to identify the basic redundancy requirements in the design architecture of control systems that provide very high levels of mission reliability.
Meta TagsDetails
DOI
https://doi.org/10.4271/821398
Pages
12
Citation
McGlone, M., Miller, R., Davies, W., and Adams, P., "FULL AUTHORITY FAULT TOLERANT ELECTRONIC ENGINE CONTROL SYSTEMS FOR ADVANCED HIGH PERFORMANCE ENGINES (FAFTEEC)," SAE Technical Paper 821398, 1982, https://doi.org/10.4271/821398.
Additional Details
Publisher
Published
Feb 1, 1982
Product Code
821398
Content Type
Technical Paper
Language
English