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Highly integrated digital engine control system on an f-15 airplane
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Haering Jr., E. A. Burcham Jr., F. W. |
| Copyright Year | 1984 |
| Description | The Highly Integrated Digital Electronic Control (HIDEC) program will demonstrate and evaluate the improvements in performance and mission effectiveness that result from integrated engine/airframe control systems. This system is being used on the F-15 airplane. An integrated flightpath management mode and an integrated adaptive engine stall margin mode are implemented into the system. The adaptive stall margin mode is a highly integrated mode in which the airplane flight conditions, the resulting inlet distortion, and the engine stall margin are continuously computed; the excess stall margin is used to uptrim the engine for more thrust. The integrated flightpath management mode optimizes the flightpath and throttle setting to reach a desired flight condition. The increase in thrust and the improvement in airplane performance is discussed. |
| File Size | 690706 |
| Page Count | 13 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19840016519 |
| Archival Resource Key | ark:/13960/t3033pj3p |
| Language | English |
| Publisher Date | 1984-06-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Propulsion And Power Performance Tests Flight Optimization Engine Airframe Integration Uplinking Airborne/spaceborne Computers Performance Prediction Flight Paths Computerized Simulation Flight Control Systems Integration Computer Programs Flight Characteristics Aerodynamic Stalling Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
