Attitude control system is investigated assuming that satellite can be analyzed as thin circular plate; certain types of orbiting telescopes fall in this category; modes of vibration of system are determined and their influence on performance quality of three-axis control system is studied; it is shown that elastic motions are reflected on only one axis of vehicle with proper location of sensors, and that control system can be made insensitive to two lowest vibration modes; interaxis coupling has negligible influence on system stability if control system for each axis is properly designed.


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    Titel :

    Attitude control problem for flexible satellites


    Weitere Titelangaben:

    SAE-NASA -- Proc


    Beteiligte:

    Kongress:

    Proceedings of Society of Automotive Engineers, National Aeronautics and Space Administration -- Aerospace Vehicle Flight Control Conference ; 1965 Control



    Erscheinungsdatum :

    1965


    Format / Umfang :

    11 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    The Attitude Control Problem for Flexible Satellites

    Greensite, Arthur L. | SAE Technical Papers | 1965


    Attitude control of flexible communications satellites

    AGRAWAL, BRIJ / GRAN, RICHARD | AIAA | 1991


    On-off attitude control of flexible satellites

    SKAAR, S. B. / TANG, L. / YALDA-MOOSHABAD, I. | AIAA | 1986


    Satellites attitude control system

    GRIGALIUNAS VALDAS / VILKAUSKAS ANDRIUS / KARPAVICIUS ALGIS et al. | Europäisches Patentamt | 2021

    Freier Zugriff

    SATELLITES ATTITUDE CONTROL SYSTEM

    GRIGALIUNAS VALDAS / VILKAUSKAS ANDRIUS / KARPAVICIUS ALGIS et al. | Europäisches Patentamt | 2021

    Freier Zugriff