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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    Title :

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


    Publication date :

    1987


    Size :

    324 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English