Shuttle Main Engine Model I dent if ication

نویسندگان

  • Ahmet Duyar
  • Ten-Huei Guo
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.

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تاریخ انتشار 2004