H∞ control design for a jet engine

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

Volumn , Issue , 1998, Pages

  Adibhatla, Shrider ^a   Collier, George J ^a   Zhao, Xin ^a   Frederick, Dean ^b   Garg, Sanjay ^c  

^a GE AVIATION   (United States)

^b Albany Technology Services   (United States)

^c NASA GLENN RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ENGINES; GRAPHICAL USER INTERFACES; JET ENGINES; PROPULSION; USER INTERFACES;

GAIN SCHEDULING TECHNIQUES; INTEGRATOR WINDUP; LINEAR AND NONLINEAR MODELS; MAINTENANCE PROCESS; MULTIVARIABLE CONTROL; ORDER REDUCTION TECHNIQUES; PROTECTION SCHEMES; VARIABLE-CYCLE ENGINES;

DESIGN;

EID: 33845750976     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (15)

1. Frederick, D., Garg, S., and Adibhatla, S., “Turbofan Engine Control Design Using Robust Multivariable Control Technologies”, AIAA-96-2587, 32nd Joint Propulsion Conference, Florida, July, 1996.
2. Frederick, D. K., and Adibhatla, S., “The Application of KL and Integrator Windup Protection Control Design Algorithms to a GE Turbofan Engine”, final report prepared under NASA Lewis Large Engine Technology Task Order No.58, contract No. NAS3-26617, Dec. 1995.
3. Garg, S., “Robust Integrated Flight/Propulsion Control Design for a STOVL Aircraft Using tL, Control Design Techniques”, Automatica, Vol.29, No.1, 1993, pp. 129-145.
4. Garg, S., “A Simplified Scheme for Scheduling Multivariable Controllers and Its Application to a Turbofan Engine”, ASME International Gas Turbine Institute Expo, Birmingham, UK, June 1996. 5. 6.
5. Watts, S. R., and Garg, S., “An Optimized Integrator Protection Technique Applied to a Turbofan Engine”, NASA TM 107035, NASA Lewis Research Center, Cleveland, OH, October 1995.
6. French, M.W., “Development of a Compact Real-Time Turbofan Engine Dynamic Simulation,” SAE Paper 821401, October, 1982.
7. Edmunds, J.M., “Control System Design and Analysis Using Closed-Loop Nyquist and Bode Arrays,” International Journal of Control, Vol. 30, No. 5, 1979, pp. 773-802.
8. Maciejowski, J.M., Feedback Control Design, Addison-Wesley, 1989.
9. Policy, J.A., Adibhatla, S., and Baheti, K., “Design of Jet Engine Control System by Multivariable Frequency Domain Method,” American Control Conference, Seattle WA, Session WP10, June 18,1996.
10. Franklin, G.F., Powell, J.D., and Workman, M.L., Digital Design of Control Systems, Addison Wesley, 1990.
11. Grace, A., Laub, A. J., Little, J. N., Thompson, C. M., Control System Toolbox for Use with MATLAB, The Math Works, 1994.
12. Enns, D. F., Model Reduction for Control System Design, Ph. D. Dissertation, Stanford University, 1984.
13. Baheti, R. A., “Simple Anti-Windup Controllers”, Proceedings of the 1989 American Control Conference, Pittsburgh, PA, pp. 1684-1686.
14. Hanus, R., Kinneart, M., and Henrotte, J. L., “Conditioning Technique, A General Antiwindup and Bumpless Transfer Method”, Automatica, Vol. 23, No. 6, pp.729-739, 1987.
15. Kapoor, N. and Teel, A.R., “A Dynamic Compensation Scheme Applied to a Turbofan Engine”, 36th IEEE Conference on Decision and Control, pp. 4689-4694, 1997, San Diego, California.