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FULL AUTHORITY FAULT TOLERANT ELECTRONIC ENGINE CONTROL SYSTEMS FOR ADVANCED HIGH PERFORMANCE ENGINES (FAFTEEC)
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Abstract
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.
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Authors
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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.Also In
References
- McGlone, M. E. Davies, W. J. Miller, R. J. Smith, T. B. Dr. Peck, W. “Full Authority Fault Tolerant Electronic Engine Control Systems For Variable Cycle Engines” AFWAL TR-81-2121 December 1981
- Small, L. L. “AFWAL Turbine Engine Controls Research and Development -Present and Future” AIAA 82–0321 January 1982
- Vizzini, R. W. Lenox, T. G. Miller, R. J. “Full Authority Digital Electronic Control Turbofan Engine Demonstration” SAE # 801199 October 1980
- Avizienis, A., “A Unifying Reliability Model for Closed Fault-Tolerant Systems” Fifth Annual Fault Tolerant Computer Conference Paris, France June 1975