Problems encountered in developing a high speed trajectory data processor for the shuttle ascent and entry phases are described. The development of a 19 state acceleration filter for the processor is reported.


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    Title :

    Space Shuttle Navigation Filter Development


    Contributors:
    W. M. Lear (author)

    Publication date :

    1976


    Size :

    7 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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