Various possible systems are examined for suitability and 3, which appear more promising, are analyzed using Orbiting Astronomical Observatory as example; system which uses error rate network to provide damping is superior to other two; dynamic tracking error of less than plus or minus 0.5 sec of arc was obtained.


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    Titel :

    Study of systems using inertia wheels for precise attitude control of satellite


    Weitere Titelangaben:

    NASA -- Tech Note


    Beteiligte:
    White, J.S. (Autor:in) / Hansen, Q.M. (Autor:in)


    Erscheinungsdatum :

    1961


    Format / Umfang :

    71 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    Satellite attitude control using combination of inertia wheels and bar magnet

    Adams, J.J. / Brissenden, R.F. | Engineering Index Backfile | 1960


    SIMULATOR STUDY OF A SATELLITE ATTITUDE CONTROL SYSTEM USING INERTIA WHEELS AND A MAGNET

    Adams, J. J. / Bergeron, H. P. / Howell, W. E. | NTRS | 1963


    Inertia-Free Spacecraft Attitude Control Using Reaction Wheels

    Weiss, Avishai / Kolmanovsky, Ilya / Bernstein, Dennis S. et al. | AIAA | 2013