Evaluation of an outer loop retrofit architecture for intelligent tbrbofan engine thrust control

Collection of Technical Papers - AIAA/ASME/SAE/ASEE 42nd Joint Propulsion Conference

Volumn 9, Issue , 2006, Pages 7496-7523

  Litt, Jonathan S ^a,c,d   Sowers, T Shane ^b,e  

^a NASA GLENN RESEARCH CENTER   (United States)

^b ANALEX CORPORATION   (United States)

^c Vehicle Technology Directorate   (United States)

^d AIAA   (United States)

^e NONE   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ENGINE CONTROL; LOOP THRUST CONTROL; OPERATING POINTS; THRUST ESTIMATION;

COMPUTER SIMULATION; CONTROL SYSTEM APPLICATIONS; RETROFITTING; ROBUSTNESS (CONTROL SYSTEMS);

TURBOFAN ENGINES;

EID: 34249338675     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (12)

1. Litt, J. S., et al., "A Survey of Intelligent Control and Health Management Technologies for Aircraft Propulsion Systems," Journal of Aerospace Computing, Information, and Communication [online journal], Vol. 1, No. 12, December 2004, pp. 543-563, URL: www.aiaa.org/jacic/. [cited 2 September 2005].
2. Litt, J. S., Turso, J. A., Shah, N., Sowers, T. S., and Owen, A. K., "A Demonstration of a Retrofit Architecture for Intelligent Control and Diagnostics of a Turbofan Engine," Infotech@ Aerospace, Arlington, VA , 26-29 Sept, 2005.
3. Martucci, A., and Volponi, A.J., "Fuzzy Fuel Flow Selection Logic for a Real Time Embedded Full Authority Digital Engine Control," Journal of Engineering for Gas Turbines and Power, Vol. 125, Oct. 2003, pp. 909-916.
4. Bosco, C. J., "Certification Issues For Electrical and/or Electronic Engine Controls," SAE Paper 871844, Aerospace Technology Conference and Exposition, Long Beach, CA, Oct. 5-8, 1987.
5. Litt, J. S., "An Optimal Orthogonal Decomposition Method for Kalman Filter-Based Turbofan Engine Thrust Estimation," GT2005-68808, Proceedings of the 2005 ASME Turbo Expo, Reno-Tahoe, NV, June 6-9, 2005.
6. Volponi, A. J., "Gas Turbine Parameter Corrections," Journal of Engineering for Gas Turbines and Power, Vol. 121, October 1999, pp. 613-621.
7. Kurzke, J., "Model Based Gas Turbine Parameter Corrections," GT203-38234, Proceedings of 2003 ASME Turbo Expo, June 16-19, 2003.
8. Kobayashi, T., Simon, D. L., "Evaluation of an Enhanced Bank of Kalman Filters for In-Flight Aircraft Engine Sensor Fault Diagnostics," Journal of Engineering for Gas Turbines and Power, Vol. 127, July 2005, pp. 497-504.
9. nd, Instrument Society of America, Research Triangle Park, NC, 1995, pp. 88-91.
10. The Aircraft Gas Turbine Engine and its Operation, Part No. PWA 182408, PWA Oper. Instr. 200, United Technologies Corporation, Reprinted with revisions August 1988.
11. Brunell, B. J., Viassolo, D. E., and Prasanth, R., "Model Adaptation and Nonlinear Model Predictive Control of an Aircraft Engine," GT-2004-53780, Proceedings of the 2004 ASME Turbo Expo, Vienna, Austria, 2004.
12. Brotherton, T., Volponi, A., Luppold, R., and Simon, D.L., "eSTORM: Enhanced Self Tuning On-board Real-time Engine Model," Proceedings of the 2003 IEEE Aerospace Conference, Big Sky, MT, March 8-15, 2003.