Synthesis of specific optimum control law for stabilization of satellite; it is shown that specific optimum control law yields acceptable performance while being much easier to instrument than optimum control law.


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    Titel :

    Stabilization of satellite via specific optimum control


    Weitere Titelangaben:

    IEEE -- Trans Aerospace Electronic System


    Beteiligte:
    Kumar, K.S.P. (Autor:in) / Teng, L. (Autor:in)


    Erscheinungsdatum :

    1966


    Format / Umfang :

    4 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Stabilization of a Satellite via Specific Optimum Control

    Kumar, K. S. P. / Teng, Lincoln | IEEE | 1966


    On optimum stabilization of satellite

    Kumar, K.S.P. | Engineering Index Backfile | 1965


    On the Optimum Stabilization of a Satellite

    Kumar, K. S. P. | IEEE | 1965


    Optimum Ship Steering-Stabilization Control

    Whalley, R. | Online Contents | 2003


    Optimum launching of satellite by two impulses of unequal specific impulse

    Ting, L. / Pierucci, M. | Engineering Index Backfile | 1963