The Digital Electronic Engine Control (DEEC) system considered is a relatively low cost digital full authority control system containing selectively redundant components and fault detection logic with capability for accommodating faults to various levels of operational capability. The DEEC digital control system is built around a 16-bit, 1.2 microsecond cycle time, CMOS microprocessor, microcomputer system with approximately 14 K of available memory. Attention is given to the control mode, component bench testing, closed loop bench testing, a failure mode and effects analysis, sea-level engine testing, simulated altitude engine testing, flight testing, the data system, cockpit, and real time display.
Flight test of a full authority Digital Electronic Engine Control system in an F-15 aircraft
Joint Propulsion Conference ; 1981 ; Colorado Springs, CO, US
01.07.1981
Aufsatz (Konferenz)
Keine Angabe
Englisch
Full Authority Digital Electronic Control Turbofan Engine Demonstration
SAE Technical Papers | 1980
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