For purposes of parameter identification, a class of N-degree of freedom dynamical systems are decoupled, to a single degree of freedom subsystem. This is achieved by utilizing all measured accelerations, and a coordinate transformation. In cases where additional data of strains or displacements are available, the decoupled equations are further simplified. The merits of this decoupling are clearly indicated.


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    Title :

    Identification of Structural Component Failures Under Dynamic Loading


    Additional title:

    Sae Technical Papers


    Contributors:

    Conference:

    Aerospace Meeting ; 1977



    Publication date :

    1977-02-01




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English





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