The TIROS-N television infrared observatory system is discussed. The characteristics of the primary payload sensor are presented. The attitude control system jitter specification for satisfactory performance of the sensor is analyzed. The primary sensor is the advanced very high resolution radiometer. The TIROS-N satellite is an orbital platform carrying a number of earth observation sensors. The requirements for three axis attitude control for proper positioning of the sensors are reported. (Author)


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    Titel :

    Tiros-n Spacecraft Jitter Calculations


    Beteiligte:
    G. M. Fleisher (Autor:in)

    Erscheinungsdatum :

    1972


    Format / Umfang :

    14 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    TIROS-N spacecraft jitter calculations

    Fleisher, G. M. | NTRS | 1972


    TIROS OPERATIONS

    Powers, E. F. | NTRS | 1963


    TIROS ACHIEVEMENTS

    Rados, R. M. | NTRS | 1963


    Tiros meteorological operations

    Jones, J.B. / Mace, L.M. | Engineering Index Backfile | 1963


    Tiros Program Results

    Tepper, M. | NTRS | 1961