The purpose of the Flight Experiment Demonstration System (FEDS) was to show, in a simulated spacecraft environment, the feasibility of using a microprocessor to automate the onboard orbit determination functions. The software and hardware configuration used to support FEDS during the demonstration and the results of the demonstration are discussed.


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    Titel :

    Flight Experiment Demonstration System (FEDS) analysis report


    Beteiligte:
    Shank, D. E. (Autor:in)

    Erscheinungsdatum :

    1986-07-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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