This paper provides an overview of the on-orbit operation of the Attitude Control Subsystem (ACS) for the Advanced Communications Technology Satellite (ACTS). The three ACTS control axes are defined, including the means for sensing attitude and determining the pointing errors. The desired pointing requirements for various modes of control as well as the disturbance torques that oppose the control are identified. Finally, the hardware actuators and control loops utilized to reduce the attitude error are described.


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    Titel :

    Attitude Control Subsystem for the Advanced Communications Technology Satellite


    Beteiligte:
    A. W. Hewston (Autor:in) / K. A. Mitchell (Autor:in) / J. T. Sawicki (Autor:in)

    Erscheinungsdatum :

    1996


    Format / Umfang :

    31 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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