Response relations, vehicle attitude, control torque, wheel motion, mechanical power, and energy consumption for space vehicle subjected to sinusoidal or impulsive disturbances; resulting normalized numerical relations serve as order of magnitude basis for preliminary design estimates and comparisons; response relations are derived for single axis model; applicability to 3-axis design; control system proposed decouples vehicle dynamics so that motions are exactly single axis.


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    Titel :

    Some basic response relations for reaction-wheel attitude control


    Weitere Titelangaben:

    ARS J


    Beteiligte:

    Erschienen in:

    ARS Journal ; 32 , n 1 ; p 61-74


    Erscheinungsdatum :

    1962


    Format / Umfang :

    14 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    Basic response relations for attitude control using gyros

    Cannon, Jr., R.H. | Engineering Index Backfile | 1963


    Basic response relations for satellite attitude control using gyros

    Cannon, Jr., R.H. | Engineering Index Backfile | 1964