Survey of state of art and present use of control moment gyros; fundamentals of systems, derivation of equations for promising configurations, and problems encountered in some space vehicle attitude control applications; techniques generated to overcome these and predictions of high accuracy performance from analog computer and air-bearing simulator studies are presented; systems are capable of controlling spinning or nonspinnig vehicles and may be used in active or semipassive mode; simple two-degree-of-freedom coning suspension gimbal structure that retains and possesses no major gyroscopic cross-coupling is proposed.


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    Titel :

    Control moment gyros in attitude control


    Weitere Titelangaben:

    J Spacecraft Rockets


    Beteiligte:
    Jacot, A.D. (Autor:in) / Liska, D.J. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1966


    Format / Umfang :

    8 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    Control moment gyros in attitude control.

    JACOT, A. D. / LISKA, D. J. | AIAA | 1966




    Precision Attitude Control of Spacecraft with Control Moment Gyros

    Taniwaki, Shigemune / Ohkami, Yoshiaki | AIAA | 2006