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- W2972956724 abstract "This paper studies the problem of extracting turbofan engine baseline model by using FDR(Flight Data Recorder) in application. Turbofan engine baseline model extraction contains four steps: parameters analysis related to the turbofan engine baseline model, data preprocessing, identify steady state operating points of engine in the cruise phase and model fitting. The more of the engine steady state, the higher of the reliability and accuracy of the baseline model. In traditional method, only an average value of the steady state in cruise is identified. There is only one stable operation state in each flight which is applied in engine baseline model. And it reduces the credibility of baseline model fitting. This paper focuses on the steady state operating criteria of engine and the algorithm of steady state operating points identification in cruise. It solves the problem of lacking steady state operating conditions in traditional method." @default.
- W2972956724 created "2019-09-19" @default.
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- W2972956724 date "2019-06-01" @default.
- W2972956724 modified "2023-09-29" @default.
- W2972956724 title "Turbofan Engine Baseline Model Extraction Based on FDR Data" @default.
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- W2972956724 doi "https://doi.org/10.1109/ccdc.2019.8833387" @default.
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