NASA has proposed to put a Space Station in orbit in the early 1980s. This paper describes the steps involved in applying maximum likelihood estimation (MLE) method to indentify the parameters of the dynamic model of thr Space Station. The amount of computation in the MLE approach is reduced by using the method of successive approximation. Numerical results based on simulated data is presented in the paper.


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    Title :

    Indentification of Space Station Dynamics


    Additional title:

    Indentifizierung des dynamischen Verhaltens von Raumstationen


    Contributors:
    Sridhar, B. (author)


    Publication date :

    1985


    Size :

    2 Seiten, 3 Bilder, 1 Tabelle, 3 Quellen


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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