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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    Title :

    Flight Experiment Demonstration System (FEDS) analysis report


    Contributors:

    Publication date :

    1986-07-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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