Computational models for the flight experiment demonstration system (FEDS) code 580 were developed. The FEDS is a modification of the automated orbit determination system which was developed during 1981 and 1982. The purpose of FEDS is to demonstrate, in a simulated spacecraft environment, the feasibility of using microprocessors to perform onboard orbit determination with limited ground support.


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    Titel :

    Flight Experiment Demonstration System (FEDS): Mathematical Specification


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

    Erscheinungsdatum :

    1984


    Format / Umfang :

    96 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch