A low-cost single-axis pointing control system is currently being developed for the CIRRIS-82 Space Shuttle Program. This system is essentially self-contained and requires a minimum of interfacing with the host vehicle to perform the rudimentary step-hold maneuver patterns. A more advanced two-axis system is designed for future CIRRIS missions to perform more complex stare and scan maneuvers. Both systems use a microprocessor controller.


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    Titel :

    Cryogenic Infrared Radiance Instrumentation For Shuttle (CIRRIS) Pointing Control System


    Beteiligte:

    Kongress:

    Shuttle Pointing of Electro-Optical Experiments ; 1980 ; Los Angeles,United States


    Erschienen in:

    Erscheinungsdatum :

    03.04.1981





    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Cryogenic Infrared Radiance Instrumentation For Shuttle (CIRRIS)

    Smith, D. R. / Stair, A. T. / Steed, A. J. et al. | SPIE | 1981


    CIRRIS--A Cryogenic Infrared (IR) Radiance Instrument for Shuttle

    M. Ahmadjian / D. R. Smith / A. T. Stair et al. | NTIS | 1981


    CIRRIS--A Cryogenic Infrared (IR) Radiance Instrument For Shuttle

    Ahmadjian, M. / Smith, D. R. / Stair, A. T. et al. | SPIE | 1981


    CIRRIS-1A Space Shuttle experiment

    AHMADJIAN, M. / NADILE, R. M. / WISE, J. O. et al. | AIAA | 1990


    The CIRRIS experiment

    STAIR, JR., A. / SMITH, D. | AIAA | 1981