Model-based intelligent digital engine control (MoBIDEC)

33rd Joint Propulsion Conference and Exhibit

Volumn , Issue , 1997, Pages

  Adibhatla, Shrider ^a   Lewis, Timothy J ^a  

^a AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CONTROL THEORY; GAS TURBINES; NONLINEAR ANALYSIS; PROPULSION;

ADVANCED TECHNOLOGY; CLOSED-LOOP CONTROL; DERIVED PARAMETERS; DIGITAL ENGINE CONTROL; MODEL BASED CONTROLS; MODEL-BASED CONTROL SYSTEMS; PERFORMANCE BENEFITS; SIMULATION TESTING;

ENGINES;

EID: 84962786676     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (18)

1. Adibhatla, S. and Gastineau, Z., “Intelligent Engine Control (IEC),” A1AA-92-3484, 28th Joint Propulsion Conference, July, 1992.
2. Qi, O.F. and Maccalum, N.R.L., “A Model- Based Approach to the Control of a Gas Turbine Engine,” ASME Paper 93-GT-402, IGTI Aeroengine Congress and Exposition, Cincinnati OH, May, 1993.
3. French, M.W., “Development of a Compact Real-Time Turbofan Engine Dynamic Simulation,” SAE Paper 821401, October, 1982.
4. Adibhatla, S. and Gastineau, Z., “Tracking Filter Selection and Control Mode Selection for Model-Based Control,” AIAA-94-3404, 30th Joint Propulsion Conference, Indianapolis IN, June 27-29, 1994.
5. Espana, M.D., “On the Estimation Algorithm for Adaptive Performance Optimization of Turbofan Engines,” AIAA-93-1823,29th Joint Propulsion Conference, June, 1993.
6. Pineo, F.J., “Adaptive Update Method for Embedded Real-Time Jet Engine Models, M.S. Thesis, M.I.T., February, 1985.
7. Johnson, K.L., “A Constant Gain Extended Kalman Filter for Turbofan Performance Tracking,” M.S. Thesis, U. Cincinnati, 1989.
8. Luppold, R.H., Gallops, G.W., and Kerr, L.J., “Estimating In-Flight Performance Variations Using Kalman Filter Concepts,” AIAA-89-2584, 25th Joint Propulsion Conference, Monterey CA, July 10-12, 1989.
9. Sugiyama, N., “On-Line Identification of Jet Engine,” AIAA-96-2590, 32nd Joitn Propulsion Conference, Lake Buena Vista FL, July 1-3, 1996.
10. 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.
11. 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.
12. Policy, J.A., Adibhatla, S., and Hoffman, P.J., “Multivariable Turbofan Engine Control for Full Flight Envelope Operation,” ASME Paper 88- GT-6, IGTI Aeroengine Congress and Exposition, Amsterdam, June 5-9, 1988.
13. Hanus, R., “ A New Technique for Preventing Control Windup,” Journal A, Vol. 21, No. 1, 1980, pp 15-20.
14. Hanus, R., Kinnaert, M., and Henrotte, J.L., “Conditioning Technique, A General Anti- Windup and Bumpless Transfer Method,” Automatica, Vol. 23, No. 6, November 1987, pp. 729-739.
15. Baheti, R.S., “Simple Anti-Windup Controllers”, Proceedings of the American Control Conference, pp. 1684-1686, June, 1989.
16. Shaw, P., et al., “ A Design Approach to a Performance Seeking Control,” AIAA-86-1674, 22nd Joint Propulsion Conference, June 1986.
17. Adibhatla, S. and Johnson, K.L., “Evaluation of a Nonlinear PSC Algorithm on a Variable Cycle Engine,” AIAA-93-2077, 29th Joint Propulsion Conference, June 1993.
18. Smith, R.H., Chisolm, J.D., and Stewart, J.F., “Optimizing Aircraft Performance with Adaptive, Integrated Flight/Propulsion Control,” ASME Paper 90-GT-252, IGTI Aeroengine Congress and Exposition, Brussels, Belgium, June 1990