The attitude control system is utilized in a spinstabilized space vehicle. A scanner is mounted in the vehicle for rotation with it. A signal generating device is associated with the scanner for generating a signal in response to sighting of a horizon. The signal generator is associated with a solenoid device and a gas source to forcibly vary the vehicle attitude. Celestial bodies are used in the system for determining position.


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    Titel :

    Attitude Orientation of Spin-Stabilized Space Vehicles


    Beteiligte:
    H. D. Garner (Autor:in) / H. J. E. Reid (Autor:in)

    Erscheinungsdatum :

    1965


    Format / Umfang :

    1 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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    SIMULATOR STUDIES OF SIMPLE ATTITUDE CONTROL FOR SPIN-STABILIZED VEHICLES

    Garner, H. D. / Reid, H. J. E., Jr. | NTRS | 1962



    Spin stabilized satellite's attitude analytical prediction

    Zanardi, Maria Cecília / Pereira, A. J. / Chiaradia, J. E. | BASE | 2012

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