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    타이틀 The Application of Neural Networks to the SSME Startup Transient
    저자 Claudia M. Meyer and William A. Maul
    Keyword Neural nets; Space shuttle main engine; Test firing
    URL http://gltrs.grc.nasa.gov/reports/1991/CR-187138.pdf
    보고서번호 NASA CR-187138
    발행년도 1991
    출처 NASA Glenn Research Center
    ABSTRACT Feedforward neural networks were used to model three parameters during the Space Shuttle Main Engine startup transient. The three parameters were the main combustion chamber pressure, a controlled parameter; the high pressure oxidizer turbine discharge temperature, a redlined parameter; and the high pressure fuel pump discharge pressure, a failureindicating performance parameter. Network inputs consisted of time windows of data from engine measurements that correlated highly to the modeled parameter. A standard backpropagation algorithm was used to train the feedforward networks on two nominal firings. Each trained network was validated with four additional nominal firings. For all three parameters, the neural networks were able to accurately predict the data in the validation sets as well as the training set.

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