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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    Title :

    Identification of Space Shuttle Main Engine Dynamics


    Contributors:
    A. Duyar (author) / T. Guo (author) / W. C. Merrill (author)

    Publication date :

    1989


    Size :

    22 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Identification of Space Shuttle Main Engine dynamics

    Duyar, Ahmet / Guo, Ten-Huei / Merrill, Walter C. | NTRS | 1989


    Identification of space shuttle main engine dynamics

    Duyar, Ahmet / Guo, Ten-Huei / Merrill, Walter C. | NTRS | 1989



    Space Shuttle Main Engine

    Thompson, J. R., Jr. | NTRS | 1980


    Space Shuttle Main Engine

    Thompson, J. R., Jr. | NTRS | 1977