A preliminary evaluation of an F100 engine parameter estimation process using flight data-Reference-Cited by-同舟云学术

A preliminary evaluation of an F100 engine parameter estimation process using flight data

Published:1990-07-16 Issue: Volume: Page:
ISSN:
Container-title:26th Joint Propulsion Conference
language:
Short-container-title:

Author:

MAINE TRINDEL¹,GILYARD GLENN¹,LAMBERT HEATHER¹

Affiliation:

1. NASA, Flight Research Center, Edwards, CA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1990-1921

Reference12 articles.

1. 'ich,E.J., Shaw, P.D., Berg, D.F., Adhibatla, S., Swan, J.A., and Skira, C.A. "Performance Seeking Control for Cruise Optimizationin Fighter Aircraft," AIAA-87-1929,June 1987.

2. 2urcham,F.W., Jr., Myers, L.P., and Walsh, K.R., Flight Evaluation Resultsfor a Digital Electronic Engine Control in an F-15Airplane, NASA TM-84918,1983.

3. Myers, L.P., and Burcham,F.W., Jr., Preliminary Flight Test Results of the FlOO EMD Engine in an F-15Airplane,NASATM-85902,1984.

4. 4aer-iedhart, JenniferL., and Landy,Robert J., HighlyIntegrated Digital Electronic Control-Digital Flight Control, Aircraft Model Identification and AdaptiveEngineControl,NASATM-86793,1987.

5. Fan Compressor Facility,Edwards,CaliforniaMay 25-26, 1983,DigitalElectronicEngineControl(DEEC)FlightEvaluationinanF-15Airplane,NASA CP-2298.

Cited by 4 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Aero-engine direct thrust control based on nonlinear model predictive control with composite predictive model;International Journal of Turbo & Jet-Engines;2024-06-27

2. A new schedule method for compact propulsion system model;International Journal of Turbo & Jet-Engines;2024-02-09

3. In-flight performance diagnostic capability of an adaptive engine model;28th Joint Propulsion Conference and Exhibit;1992-07-06

4. Preliminary flight evaluation of an engine performance optimization algorithm;27th Joint Propulsion Conference;1991-06-24