The Command and Data Subsystem (CDS) on Cassini is responsible for uplink command processing, spacecraft intercommunications and control, and downlink telemetry formatting. The 10.7 year mission life, 160 minute round-trip light time, and extended periods of operation without continuous ground communications drive the CDS design in directions of redundancy, autonomy, and fault protection to accomodate the mission objectives.


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    Titel :

    Fault Protection Design for the Command and Data Subsystem on the Cassini Spacecraft


    Beteiligte:

    Erscheinungsdatum :

    31.10.1994


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Fault Protection Design of the Command and Data Subsystem on the Cassini Spacecraft

    Brown, T. K. / Donaldson, J. A. / IEEE et al. | British Library Conference Proceedings | 1994




    Fault Protection Architectures for the Command and Data Subsystem on the Cassini Spacecraft

    Brown, T. K. / Donaldson, J. A. / IEEE et al. | British Library Conference Proceedings | 1995