Shuttle Main Engine Model I dent if ication
نویسندگان
چکیده
System identification techniques are used to represent the dynamic behavior of the space shuttle main engine. The transfer function matrices of the linearized models of both the closed loop and the open loop system are obtained by using the recursive maximum likelihood method.
منابع مشابه
Implementation of a Model Based Fault Detection and Diagnosis for Actuation Faults of the Space Shuttle Main Engine _=_-
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تاریخ انتشار 2004