Study of attitude control of spinning satellites in circular earth orbits by means of single, onboard, current-carrying coil; interaction between controlled current and earth's magnetic field produces control torques required to precess spin axis; new feedback control law, including provisions for active magnetic nutation damping, is presented; feasibility of magnetic control for spinning vehicles is shown by verifying that control law is applicable for any desired spin-axis orientation.


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    Titel :

    Spinning spacecraft attitude control via environmental magnetic field


    Weitere Titelangaben:

    J Spacecraft Rockets


    Beteiligte:
    Wheeler, P.C. (Autor:in)

    Erschienen in:

    Journal of Spacecraft and Rockets ; 4 , n 12 ; p 1631-1637


    Erscheinungsdatum :

    1967


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :