The application of neural networks to the SSME startup transient

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...

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Bibliographische Detailangaben

Hauptverfasser:	Meyer, Claudia M., Maul, William A.
Format:	Tagungsbericht
Sprache:	eng
Schlagworte:	Launch Vehicles And Space Vehicles
Online-Zugang:	Volltext bestellen
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