Vertically oriented satellites instrumenting orbital plane exhibit certain gyroscopic properties; if one or more integrating gyroscopes are properly installed, characteristic may be used to accomplish semipassive damping of vehicle librations; vehicle oscillations cause gimbal precession in gyroscopes; damping occurs because of energy dissipation as heat in viscous restraint of each gyro; systems described comprise only gyro or gyros, properly supplied with constant power; neither external error sensing nor on-board computation is required.


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    Titel :

    Attitude control of satellites using integrating gyroscopes


    Weitere Titelangaben:

    Am Astronautical Soc -- Advances Astronautical Sciences


    Beteiligte:
    DeLisle, J.E. (Autor:in) / Ogletree, G. (Autor:in) / Hildebrant, B.M. (Autor:in)


    Erscheinungsdatum :

    1962


    Format / Umfang :

    28 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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    Three-Axis Attitude Estimation Using Rate-Integrating Gyroscopes

    Crassidis, John L. / Markley, F. Landis | AIAA | 2017