High stability engine control (HISTEC)

32nd Joint Propulsion Conference and Exhibit

Volumn , Issue , 1996, Pages

  Delaat, John C ^a   Southwick, Robert D ^b   Gallops, George W ^b  

^a NASA GLENN RESEARCH CENTER   (United States)

^b United Technologies   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT ENGINES; ENGINES; FLIGHT CONTROL SYSTEMS; INDUSTRIAL MANAGEMENT; INFORMATION MANAGEMENT; PROPULSION; STABILITY;

AIRCRAFT TURBINE ENGINES; COMPRESSOR PRESSURE RATIO; DISTORTION ESTIMATION; DISTORTION TOLERANT; ENGINE CONTROL SYSTEM; FLIGHT DEMONSTRATION; HARDWARE AND SOFTWARE; SIMULATION STUDIES;

CONTROL SYSTEM STABILITY;

EID: 85088353512     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1996-2586     Document Type: Conference Paper

References (10)

1. Longley, J.P.; and Greitzer, E.M.: “Inlet Distortion Effects in Aircraft Propulsion System Integration.” In AGARD, Steady State and Transient Performance Prediction of Gas Turbine Engines, May 27-28, 1992
2. Ralph, J.A.: Advanced Control for Airbreathing Engines, Volume 1, Pratt & Whitney.” NASA CR 189203, July 1993.
3. Bough, R.M.: Advanced Control for Airbreathing Engines, Volume 3, Allison Gas Turbine.” NASA CR 189205, July 1993
4. Ouzts, P.J.; Lorenzo, C.F.; and Menill, W.C.: “Screening Studies of Advanced Control Concepts for Airbreathing Engines.” Prepared for the 28th Joint Propulsion Conference and Exhibit, July 6-8, 1992, NASA TM 106042.
5. Eveker, K.M.; Gysling, D.L.; Nett, C.N.; and Sharrna, O.P.: “Integrated Control of Rotating Stall and Surge in Aeroengines.” In proceedings: SPJJE's International Symposium on Aerospace/Defense Sensing & Control and Dual-Use Photonics “AeroSense”, 4/17-4/21/95. Proceedings volume 2494.
6. Berndt, R.G.; Weigl, H.J.; Paduano, J.D.; and Epstein, A.H.: “Experimental Techniques for Actuation, Sensing and Measurement of Rotating Stall Dynamics in High Speed Compressors.” In proceedings: SPIEs International Symposium on Aerospace/Defense Sensing & Control and Dual-Use Photonics “AeroSense”, 4/17-4/21/95. Proceedings volume 2494.
7. Myers, L.P.; Walsh K.R.: “Performance Improvements of an F-15 Airplane With an Integrated Engine-Flight Control System.” Prepared for the AIAA Fourth Flight Test Conference, May 18-20, 1988, NASA TM 100431.
8. Southwick, Robert D.; Gallops, George W.; Larkin, Louis J.; Sobanski, Kurt J.: “High Stability Engine Control (HISTEC) Phase I: Algorithm Development, Volume I: Final Report and Appendix A.” NASA CR 198399, September 1995. (Permission to use this material was granted by Sanjay Garg, June 1996.)
9. Society of Automotive Engineers: “Inlet Total Pressure Condiderations for Gas Turbine Engines”, Aerospace Information Report (AIR) 1419,1983.
10. Society of Automotive Engineers: “Gas Turbine Engine Inlet Flow Distortion Guidelines”, Aerospace Recommended Practice (ARP) 1420, 1978.