High stability engine control (HISTEC) flight test results

34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 1998, Pages

  Southwick, R D ^a   Gallops, G W ^a   Kerr, L J ^a   Kielb, R P ^a   Welsh, M G ^a   Delaat, J C ^b   Orme, J S ^c  

^a PRATT AND WHITNEY   (United States)

^b NASA GLENN RESEARCH CENTER   (United States)

^c NASA DRYDEN FLIGHT RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ENGINES; FLIGHT CONTROL SYSTEMS; NASA; PROPULSION; REAL TIME CONTROL;

ADVANCED CONTROL; DESIGN APPROACHES; ENGINE CONTROL SYSTEM; FLIGHT RESEARCH; INLET PRESSURES; MEASUREMENT-BASED; RESEARCH CENTER; RESEARCH OBJECTIVES;

SUPERSONIC AIRCRAFT;

EID: 84963864944     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1998-3757     Document Type: Conference Paper

References (9)

1. Southwick, Robert D., George W. Gallops, Louis J. Larkin, and Kurt J. Sobanski. High Stability Engine Control (HISTEC) Phase I: Algorithm Development, Volume I: Final Report and Appendix A, NASA CR 198399, September 1995.
2. Orme, J. S., J. C. DeLaat, R. D. Southwick, G. W. Gallops, and P. M Doane. Development and Testing of a High Stability Engine Control (HISTEC) System. Paper AIAA-98-3715, presented at the 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Cleveland, July 1998.
3. DeLaat, J. C., R. D. Southwick, G. W. Gallops, and J. S. Orme. The High Stability Engine Control (HISTEC) Program: Flight Demonstration Phase. Paper AIAA-98-3756, presented at the 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Cleveland, July 1998.
4. U. S. Patent 074431 Gas Turbine Engine Control Based on Inlet Pressure Distortion. Issued September 1995, assigned to United Technologies Corporation.
5. Society of Automotive Engineers. Gas Turbine Engine Inlet Flow Distortion Guidelines, Aerospace Recommended Practice (ARP) 1420, 1978.
6. Society of Automotive Engineers. A Current Assessment of Planar Waves. Aerospace Resource Document (ARD) 50026, 1994.
7. Gong, Y., C. S. Tan, and K. A. Gordon. A Computational Model for Short Wavelength Stall Inception and Development in Multi-Stage Compressors. Paper 98-GT-476, presented at the International Gas Turbine and Aeroengine Congress and Exhibition, Stockholm, June 1998.
8. Longley, J. P., H. W. Shin, R. E. Plumley, P. D. Silkowski, I. J. Day, E. M. Greitzer, C. S. Tan, and D. C. Wisler. Effects of Rotating Inlet Distortion on Multistage Compressor Stability. ASME Journal of Turbomachinery 118, pp. 181-188, 1996.
9. DeLaat, John C., Robert D. Southwick, and George W. Gallops. High Stability Engine Control (HISTEC). Paper AIAA-96-2586, presented at the 32nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Lake Buena Vista, July 1996.