A generic system design concept for unmanned spacecraft is applied to EURECA. Allocation of autonomy requirements; system level applications; and subsystems are described. Functional and operational interfaces are discussed. Spacecraft modes of operation and the functional partitioning between the spacecraft and ground control are treated. On-board architecture; functional autonomy and on-board organization, interfaces, and the utilization of a local area network to interconnect the on-board management nodes are outlined.


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    Titel :

    Study of Standard Generic Approach for Spacecraft (S/C) Autonomy and Automation (Phase 3). Book B: Autonomy Concept Application Example


    Erscheinungsdatum :

    1987


    Format / Umfang :

    324 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch