The design concept of an inertial reference unit is reported that uses the gyroscope in a rate mode in conjunction with a unique application of a drift compensated and temperature stabilized solid state integrator for the inertial mode. A typical test program and results for an inertial reference unit as applied to the Mariner Mars 1971 program to achieve highly reliable spacecraft operation are also described. (Author)


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    Titel :

    Mariner MARS 1971 Inertial Reference Unit


    Beteiligte:
    G. T. Starks (Autor:in)

    Erscheinungsdatum :

    1974


    Format / Umfang :

    20 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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