Attitude sensing device is described which uses two narrow infrared scanning beams to provide simple means of establishing vertical reference line from orbiting space vehicle to planet under observation; device also measures several vehicle parameters, specifically, roll, pitch and yaw about local vertical, and altitude.


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    Titel :

    Attitude reference devices for space vehicle


    Weitere Titelangaben:

    IRE -- Proc


    Beteiligte:
    Kendall, P.E. (Autor:in) / Stalcup, R.E. (Autor:in)


    Erscheinungsdatum :

    1960


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Space vehicle attitude control

    Doolin, B.F. | Engineering Index Backfile | 1962


    Space Vehicle Attitude Studies

    C. D. Howard / D. J. Innes / D. Mansir | NTIS | 1968


    Space Vehicle Attitude Control

    H. C. Vivian / J. D. Acord | NTIS | 1965


    A STRAPDOWN ATTITUDE REFERENCE FOR SPACE VEHICLES

    WENNERHOLM, JR., R. | AIAA | 1966


    Space vehicle attitude control Patent

    Acord, J. D. / Vivian, H. C. | NTRS | 1965