Control of jet engines

Control Engineering Practice

Volumn 7, Issue 9, 1999, Pages 1043-1059

  Austin Spang III, H ^a   Brown, Harold ^b  

^a GE GLOBAL RESEARCH   (United States)

^b 11 Diplomat Drive   (United States)

Author keywords

Aerospace control; Computer control; Control applications; Jet engines

Indexed keywords

ACTUATORS; COMPUTATIONAL COMPLEXITY; COMPUTER CONTROL SYSTEMS; CONSTRAINT THEORY; CONTROL SYSTEM ANALYSIS; JET ENGINES; SENSORS;

AEROSPACE CONTROL;

FEEDBACK CONTROL;

AEROSPACE APPLICATION; COMPUTER CONTROL; JET ENGINE;

EID: 0344931668     PISSN: 09670661     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0967-0661(99)00078-7     Document Type: Article

References (37)

1. Adibhatla S. Propulsion control law design for the NASA STOVL controls technology program. AIAA, 93-4842, AIAA International powered lift conference. 1993;Santa Clara, CA.
2. Adibhatla, S., Cooper, P., Pajakiwski, A., Romine, B., Virnig, J., & Bodden, D. (1994). STOVL controls technology, vol. I Integrated flight/propulsion control design. NASA Contractor Report 195361.
3. Adibhatla S., Lewis T. Model-based intelligent digital engine control. AIAA 97-3192, 33rd AIAA Joint propulsion conference & exhibit. 1997;Seattle, WA.
4. ARP 755A (1974). Aerospace recommended practise. Society of Automotive Engineers.
5. Casamassa J.V., Bent R.D. Jet aircraft power systems. (3d ed.):1965;McGraw-Hill, New York.
6. Cohen H., Rogers G.F.C., Saravanamuttoo H.I.H. Gas turbine theory. (4th ed.):1996;Longman, Essex.
7. Constant II E.W. The origins of the Turbojet revolution. 1980;John Hopkins Univ. Press, Baltimore, MD.
8. Dadd, G. J., Sutton, A. E., & Greig, A. W. M. (1995). Multivariable control of military engines. Proceedings of advanced aero-engine concepts and controls, Defense Research Agency, Farnborough, England, AGARD Presentation, Seattle WA, 28-1-28-11.
9. Day, I. J. (1991). Active suppression of rotating stall and surge in axial compressors. International gas turbine and aeroengine congress and exposition. ASME Paper 91-GT-87.
10. DeHoff, R. L., Hall Jr., W. E., Adams, R. J., & Gupta, N. K. (1977). F100 multivariable control synthesis program, vol I and II. Wright Patterson Airforce Base Advanced Propulsion Lab. Report, AFAPL-TR-77-35, Dayton, OH.
11. DeHoff R.L., Hall W.E. Jr. Multivariable quadratic synthesis of an advanced turbofan engine controller. Journal of Guidance and Control. I:1978;136-142.
12. DeHoff, R. L., & Hall Jr., W. E. (1978b). Multivariable control design principles applied to a variable cycle turbofan engine. Proceedings of the asilomer conference on circuits, systems, and computers (pp. 122-131) CA: Pacific Grove.
13. DeHoff R.L., Hall W.E. Jr. Optimal control of turbine engines. Journal of Dynamic Systems. Measurements and Controls. 101:1979;117-126.
14. Dwyer, W. J. (1990). Adaptive model-based control applied to a turbofan aircraft engine. MA: Cambridge, MSc thesis, Department of Mechanical Eng., MIT.
15. Epstein A.H., Ffowcs-Williams J.E., Greitzer E.M. Active suppression of aerodynamic instabilities in turbomachines. Journal of Propulsion and Power. 5(2):1989;204-211.
16. Eveker, K. M., Gysling, D. L., Nett, C. N., & Sharma, O. P. (1995). Integrated control of rotating stall and surge in aeroengines. Proceedings of sensing, actuation, and control in aeropropulsion conference, FL: Orlando, SPIE Proceedings, vol. 2494 (pp. 21-35).
17. Gilmore Jr., D. R. (1992). Two decades of T700 control system growth. Proceedings of the fourth CASI symposium on propulsion (pp. 15-25).
18. Gutmark, E. J., Parr, T. P., Wilson, K. J., Schadow K. C. (1995). Active control in combustion systems with vortices. Proceedings of fourth IEEE conference on control applications (pp. 679-684). NY: Albany.
19. Gutmark E.J., Parr T.P., Wilson K.J., Yu K.H., Smith R.A., Harrisonparr D.M., Schadow K.C. Compact waste incinerator based on vortex combustion. Combustion Science and Technology. 121:1996;333-349.
20. Hanus R., Kinnaert M., Henrotte J.L. Conditioning technique, a general anti-windup and bumpless transfer method. Automatica. 23:1987;729-739.
21. Hoffmann L.G., Teper G.L., Whitbeck R.F. Application of frequency domain multivariable control synthesis techniques to an illustrative problem in jet engine control. Sain M.K., Peczkowski J.L., Melsa J.L. Alternatives for linear multivariable control with turbofan engine theme problem. 1978;51-70 Nat. Eng. Consortium, Chicago.
22. Kapoor, N., Teel, A. R. (1997). A dynamic windup compensation scheme applied to a turbofan engine. 36th IEEE Conference on decision and control proceedings (pp. 4689-4694). CA: San Diego.
23. Kouvaritakis B., Edmunds J.M. The characteristic frequency and characteristic gain design method for multivariable feedback systems. Sain M.K., Peczkowski J.L., Melsa J.L. Alternatives for linear multivariable control with turbofan engine theme problem. 1978;229-246 Nat. Eng. Consortium, Chicago.
24. MacFarland, A. G. J., McMorran, P. D., Dixon, B. A., & Hodge, S. S. (1971). Application of multivariable control techniques to aircraft gas turbines. Conference on multivariable control systems design and application.
25. McMorran P.D. Design of gas-turbine controller using inverse Nyquist method. Proceedings of IEE. 117:1970;2050-2058.
26. Mordoff K. General electric flies first unducted fan demonstrator. Aviation Week and Space Technology. 125:1986;31.
27. Oates G.C. Aerothermodynamics of gas turbine and rocket propulsion, revised and enlarged. 1988;American Institute of Aeronautics and Astronautics, Washington, DC.
28. Parsons, D. A. (1991). N-dot schedules dynamic compensation system for gas turbines - inputs sum of speed and rate of change of speed of gas generator to schedule to output desired acceleration as function of generator speed. U.S. Patent 5029441.
29. Peczkowski J.L., Sain M.K. Linear multivariable synthesis with transfer functions. Sain M.K., Peczkowski J.L., Melsa J.L. Alternatives for linear multivariable control with turbofan engine theme problem. 1978;71-87 Nat. Eng. Consortium, Chicago.
30. Rock, S. M., & De Hoff, R. L. (1979). Variable cycle engine multivariable control synthesis. Wright Patterson Airforce Base Advanced Propulsion Lab. Report, AFAPL-TR-79-2043, Dayton OH.
31. Sain, M. K., Peczkowski, J. L., & Melsa, J. L. (eds.). (1978). Alternatives for linear multivariable control with turbofan engine theme problem. Chicago: Nat. Eng. Consortium.
32. Skira, C. J., DeHoff, R. L., & Hall Jr., W. E. (1979). Design, evaluation and test of an electronic, multivariable control for the F100 turbofan engine, AGARD-PP-274, Advanced Control System for Aircraft Power, Cologne, Germany, 10-1-10-20.
33. Smith G.G. Gas turbines and jet propulsion. 1955;Philosophical Library, New York.
34. Spang III H.A. Insight into the application of the inverse nyquist array method. Sain M.K., Peczkowski J.L., Melsa J.L. Alternatives for linear multivariable control with turbofan engine theme problem. 1978;138-155 Nat. Eng. Consortium, Chicago.
35. St. John, D., Samuelson, S. (1995). Optimal, active control of oxides of nitrogen (NOx) emissions from a natural gas-fired burner using a simple genetic algorithm. Proceedings of fourth IEEE conference on control applications (pp. 673-678) NY: Albany. NY.
36. Treager I.E. Aircraft Gas Turbine Engine Technology. 2nd Edition:1979;McGraw-Hill, New York.
37. Zeller, J.B., Lehtinen, & Merrill, W. (1982). The role of modern control theory in the design of controls for aircraft turbine engines. NASA Tech. Memo. 82815, Lewis Research Center, Cleveland, OH. Also in AIAA twentieth aerospace sciences conference, Orlando, FL, 1982 (pp. 11-14).