Fundamental aspects of problem of controlling attitude of satellite are considered illustrating factors involved by reference to program of attitude control development in Elliott-Automation; basic concept in control system is control loop itself; as example, control loop from Stage 1 attitude control for Skylark sounding rocket is shown; design considerations for components of control loop are considered, in particular, Sun sensor, signal processor module, and actuator system; propane control system installed in Skylark nose cone is also described.


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    Titel :

    Attitude control of sun-pointing scientific satellites


    Weitere Titelangaben:

    Spaceflight


    Beteiligte:
    Cope, P.E.G. (Autor:in)

    Erschienen in:

    Spaceflight ; 9 , n 2


    Erscheinungsdatum :

    1967


    Format / Umfang :

    3 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :