An expert system approach to turbopump health monitoring

Author:

PERRY JOHN1,RIECHEL JAY1,NORMAN ARNIE1,MADSZAR GEORGE2

Affiliation:

1. Rockwell International Corp., Rocketdyne Div., Canoga Park, CA

2. NASA, Lewis Research Center, Cleveland, OH

Publisher

American Institute of Aeronautics and Astronautics

Cited by 5 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. Predictive Health Status Assessment of a Launch Vehicle Engine in an Ascending Flight Based on Vibration Signals;IEEE Transactions on Aerospace and Electronic Systems;2023-12

2. A Multilayered and Multifactorial Health Assessment Method for Launch Vehicle Engine under Vibration Conditions;Aerospace;2023-05-27

3. Visualization analysis of rocket fault detection technology based on Citespace;2021 8th International Conference on Information, Cybernetics, and Computational Social Systems (ICCSS);2021-12-10

4. Model-based diagnosis of the space shuttle main engine;Artificial Intelligence for Engineering Design, Analysis and Manufacturing;1992-08

5. PARAMETER ESTIMATION BY NONLINEAR SMOOTHING FOR FAULT MONITORING ON ROCKET ENGINES;Fault Detection, Supervision and Safety for Technical Processes 1991;1992

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